Aviat Networks IRU600V4 IRU 600v4 MP User Manual

Aviat Networks (S) Pte. Ltd IRU 600v4 MP

User Manual

EclipseUser ManualVersion 8.04.02260-668066-001
USER MANUAL260-668066-001 JULY 2018 IIICopyright & Terms of UseJuly 2018This documentation incorporates features and functions provided with Eclipse User Manual,version 8.04.02.Copyright © 2018 by Aviat Networks, Inc.All rights reserved.No part of this publication may be reproduced, transmitted, transcribed, stored in a retrievalsystem, or translated into any language or computer language, in any form or by any means,electronic, magnetic, optical, chemical, manual, or otherwise, without the prior writtenpermission of Aviat Networks Inc.To request permission, contact techpubs@aviatnet.com.WarrantyAviat Networks makes no representation or warranties with respect to the contents hereofand specifically disclaims any implied warranties or merchantability or fitness for anyparticular purpose.Further, Aviat Networks reserves the right to revise this publication and to make changesfrom time to time in the content hereof without obligation of Aviat Networks to notify anyperson of such revision or changes.Safety RecommendationsThe following safety recommendations must be considered to avoid injuries to personsand/or damage to the equipment:1. Installation and Service Personnel: Installation and service must be carried out byauthorized personnel who have the technical training and experience necessary to beaware of any hazardous operations during installation and service, and of measures toavoid any danger to themselves, to any other personnel, and to the equipment.2. Access to the Equipment: Access to the equipment in use must be restricted to servicepersonnel only.3. Safety Norms: Recommended safety norms are detailed in the Health and Safetysections of the Eclipse User Manual.4. Service Personnel Skill: Service personnel must have received adequate technicaltraining on telecommunications and in particular on the equipment and capabilities thisaddendum refers to.TrademarksAll trademarks are the property of their respective owners.
USER MANUALIV AVIAT NETWORKS
USER MANUAL260-668066-001 JULY 2018 VAviat NetworksTechnical SupportService and Technical Support:For customer service and technical support, contact one of the regional Technical HelpDesks listed below.Americas Technical Help Desk EMEA Technical Help Desk Asia Pacific Technical Help DeskAviat Networks, Inc.San Antonio, TXU.S.A.Aviat NetworksBlantyre, Glasgow, ScotlandG72 0FBUnited KingdomAviat NetworksClark Freeport ZonePhilippines 2023Phone:+1 210 526 6345Toll Free (USA):+1 800 227 8332Fax:+1 210 526 6315Phone: +1 210 526 6345Fax:+44 16 9871 7204 (English)+33 1 5552 8012 (French)Phone: +1 210 526 6345Fax: +63 45 599 5196Email: TAC.AM@aviatnet.com Email: TAC.EMEA@aviatnet.com Email: TAC.APAC@aviatnet.comGlobal Support Hotline: +1 210 526 6345Call this phone number for support from anywhere in the world. Aviat Networks' GlobalSupport Hotline is available 24 hours a day, 7 days a week, providing uninterrupted supportfor all our customers.When you call our Global Support Hotline:lYou will be greeted by an automated response that will ask you for your PIN#.Request a PIN# here: http://aviatnetworks.com/contact-us/technical-assistance/pin-request-form/.lAs soon as you enter your PIN#, you will be transferred to our Global TechnicalHelpdesk that will assist you with your technical issue.lIf you do not have a PIN# your call will be answered by our Support AssuranceDesk. Your call will be supported and prioritized accordingly.Or you can contact your local Aviat Networks office. Contact information is available on ourwebsite at: http://www.aviatnetworks.com/services/customer-support/technical-assistance/
USER MANUALVI AVIAT NETWORKSSales and Sales Support:For sales information, contact one of the Aviat Networksheadquarters, or find your regionalsales office at: HTTP://WWW.AVIATNETWORKS.COM/.Corporate HeadquartersCalifornia, USAInternational HeadquartersSingaporeAviat Networks, Inc.860 N. McCarthy Blvd., Suite 200Milpitas, CA 95035U.S.A.Phone: + 1 408 941 7100Fax: + 1 408 941 7110Toll Free for Sales Inquiries:+ 1 888 478 9669Aviat Networks (S) Pte. Ltd.51 Changi Business Park Central 2#04-10 The SignatureSingapore 486066Phone: + 65 6496 0900Fax: + 65 6496 0999>Sales Inquiries:+1-321-674-4252
USER MANUAL260-668066-001 JULY 2018 VIIProduct Compliance NotesEclipse EMC testing was completed using screened cable; if any other type of cable is used, itmay violate compliance.Eclipse is a Class A product. In a domestic environment this product may cause radiointerference in which case the user may be required to take adequate measures. Thisequipment is intended to be used exclusively in telecommunications centers.Regulatory Information for 5.8 GHz BandEclipse IRU 600The following regulatory information applies to license-free operation on the 5.8 GHz band ofIRU 600v2, IRU 600v3 and IRU 600v4.FCC NoticesIRU 600v2/v3lIRU 600, 5.8GHz, must be professionally installed and maintained.lThis equipment has been tested and found to comply with the limits for a Class Adigital device, pursuant to Part 15 of the FCC rules. These limits are designed toprovide reasonable protection against harmful interference when the equipmentis operated in a commercial environment. This equipment generates, uses andcan radiate radio frequency energy and, if not installed and used in accordancewith the instruction manual, may cause harmful interference to radiocommunications. Operation of this equipment in a residential environment islikely to cause harmful interference in which case the user will be required tocorrect the interference at their own expense.lIRU 600, 5.8GHz, is compliant with the relevant parts of FCC CFR47, Part 15.407.lTo ensure compliance with the FCC RF exposure requirements, a minimumdistance of 18 meters must be maintained between the antenna and any personswhilst the unit is operational. This calculation is based on the maximumconducted power and maximum antenna gain.lIRU600, 5.8GHz, has been certified for use with a parabolic antenna with amaximum gain of 45.9dBi or a flat panel antenna with a maximum gain of 28dBi.lThe filters and software provided with this product allow for transmission only inthe frequency range 5725 – 5850 MHz to ensure compliance with Part 15.407.lAccording to the conducted power limit in FCC CFR 47, Part 15.407, the power forthis device has been limited to 1W (30dBm) at the antenna port.lFCC CFR47, Part 15.407 excludes the use of point-to-multipoint systems,
USER MANUALVIII AVIAT NETWORKSomnidirectional applications and multiple co-located intentional radiators. Thissystem is only for fixed, point-to-point operation.IRU 600v4lIRU 600 , 5.8GHz, must be professionally installed and maintained.lThis equipment has been tested and found to comply with the limits for a Class Adigital device, pursuant to Part 15 of the FCC rules. These limits are designed toprovide reasonable protection against harmful interference when the equipmentis operated in a commercial environment. This equipment generates, uses andcan radiate radio frequency energy and, if not installed and used in accordancewith the instruction manual, may cause harmful interference to radiocommunications. Operation of this equipment in a residential environment islikely to cause harmful interference in which case the user will be required tocorrect the interference at their own expense.lIRU 600 , 5.8GHz, is compliant with the relevant parts of FCC CFR47, Part 15.407.lTo ensure compliance with the FCC RF exposure requirements, a minimumdistance of 18 meters must be maintained between the antenna and any personswhilst the unit is operational. This calculation is based on the maximumconducted power and maximum antenna gain.lIRU 600, 5.8GHz, has been certified for use with a parabolic or a flat panelantenna with a maximum gain of 43dBi.lThe filters and software provided with this product allow for transmission only inthe frequency range 5725 – 5850 MHz to ensure compliance with Part 15.407. Theminimum transmit frequency settable in software is 5742.5MHz and themaximum settable transmit frequency is 5832.5MHz.lAccording to the conducted power limit in FCC CFR 47, Part 15.407, the power forthis device has been limited to 1W (30dBm) at the antenna port.lFCC CFR47, Part 15.407 excludes the use of point-to-multipoint systems,omnidirectional applications and multiple co-located intentional radiators. Thissystem is only for fixed, point-to-point operation.lThis device complies with Part 15 of the FCC Rules. Operation is subject to thefollowing two conditions:(1) this device may not cause harmful interference, and(2) this device must accept any interference received, including interference that maycause undesired operation.lNo changes shall be made to the equipment without the manufacturer’s permissionas this may void the user’s authority to operate the equipment.ISED (Canada) NoticesIRU 600v2/v3lIRU600, 5.8GHz, must be professionally installed and maintained.lIRU600, 5.8GHz, is compliant with Industry Canada RSS-210.
USER MANUAL260-668066-001 JULY 2018 IXlTo ensure compliance with the Industry Canada RF exposure requirements inRSS-102, a minimum distance of 18 meters must be maintained between theantenna and any persons whilst the unit is operational. This calculation is basedon the maximum conducted power and maximum antenna gain.lIRU600, 5.8GHz, has been certified for use with a parabolic antenna with amaximum gain of 45.9dBi or a flat panel antenna with a maximum gain of 28dBi.lThe filters and software provided with this product allow for transmission only inthe frequency range 5725 – 5850 MHz to ensure compliance with the Canadianband edges.lAccording to the conducted power limit in RSS-210 Annex 8, the power for thisdevice has been limited to 1W (30dBm) at the antenna port.IRU 600v4lIRU 600, 5.8GHz, must be professionally installed and maintained.lIRU 600, 5.8GHz, is compliant with Industry Canada RSS-247.lTo ensure compliance with the Industry Canada RF exposure requirements in RSS-102, a minimum distance of 18 meters must be maintained between the antennaand any persons whilst the unit is operational. This calculation islbased on the maximum conducted power and maximum antenna gain.lThe filters and software provided with this product allow for transmission only inthe frequency range 5725 – 5850MHz to ensure compliance with the Canadian bandedges.lAccording to the conducted power limit in RSS-247 the power for this device hasbeen limited to 1W (30dBm) at the antenna port.lThis device complies with ISED’s license-exempt RSSs. Operation is subject to thefollowing two conditions:(1) This device may not cause interference; and(2) This device must accept any interference, including interference that may causeundesired operation of the device.lThis radio transmitter (IC: 4469A-IRU600v4) has been approved by ISED to operatewith the antenna types listed below with the maximum permissible gain indicated.Antenna types not included in this list, having a gain greater than the maximum gainindicated for that type, are strictly prohibited for use with this device. IRU 600v4,5.8GHz, has been certified for use with a parabolic or flat panel antenna with amaximum gain of 43dBi. Please see Antennas certified for use with IRU 600v4 at5.8GHz on page 125 for a list of the antennas approved for use with this radio.lUnder ISED regulations, this radio transmitter may only operate using an antennaof a type and maximum (or lesser) gain approved for the transmitter by ISED. Toreduce potential radio interference to other users, the antenna type and its gainshould be so chosen that the equivalent isotropically radiated power (e.i.r.p.) is notmore than that necessary for successful communication.
USER MANUALX AVIAT NETWORKSISDE (Canada)IRU 600v2/v3lL’IRU600, 5.8 GHz, doit être mis en oeuvre et maintenu par des professionnels.lL’IRU600, 5.8 GHz, est conforme à la spécification RSS-210 d’Industrie Canada.lPour assurer la conformité aux exigences d’exposition de la spécification RSS-102 d’Industrie Canada, une distance minimum de 18 mètres entre l’antenne ettoute personne doit être assurée quand l’équipement est en fonctionnement. Cecalcul est basé sur la puissance émise maximum et le gain maximum del’antenne.lL’IRU600, 5.8 GHz, a été homologué avec utilisation d’une antenne paraboliquede gain maximum 45.9 dBi ou d’une antenne plane de gain maximum 28 dBi.lLes filtres et le logiciel fournis avec ce produit permettent la transmission dansla bande de fréquences 5725 – 5850 MHz seulement, pour assurer la conformitéavec les limites de bande canadiennes.lEn conformité avec la limite de puissance émise de la spécification RSS-210Annexe 8, la puissance de cet équipement a été limitée à 1 W (30dBm) à l’accèsde l’antenne.IRU 600v4lL’IRU 600, 5.8 GHz, doit être installé et maintenu par des professionnels.lL’IRU 600, 5.8 GHz, est conforme à la spécification RSS-247 de l’Industrie duCanada.lPour assurer la conformité aux exigences d’exposition de la spécification RSS-102de l’Industrie du Canada, une distance minimum de 18 mètres doit être assuréeentre l’antenne et une personne, quand l’équipement est en fonctionnement. Cecalcul est basé sur la puissance émise maximum et le gain maximum de l’antenne.lLes filtres et le logiciel fournis avec ce produit permettent la transmission dans labande de fréquences 5 725 – 5 850 MHz seulement, pour assurer la conformitéavec les limites de bande canadiennes.lEn conformité avec la limite de puissance émise de la spécification RSS-247 lapuissance de cet équipement a été limitée à 1 W (30 dBm) à l’accès de l’antenne.lCet appareil est conforme aux notre RSS exemptes de licence de l'ISED. Sonutilisation est soumise aux deux conditions suivantes:(1) Cet appareil ne doit pas causer d'interférence; et(2) Cet appareil doit accepter tout type d’interférence, y compris les interférencessusceptibles de provoquer un fonctionnement indésirable de l'appareil.lCet émetteur radio (IC: 4469A-IRU600v4) a été approuvé par l’ISED pourfonctionner avec les types d'antenne listés ci-dessous avec le gain maximumadmissible indiqué. Les types d'antennes non inclus dans cette liste, ayant un gainsupérieur au gain maximal indiqué pour ce type, sont strictement interdits pour uneutilisation avec cet appareil. L'IRU 600v4, 5,8 GHz, a été certifié pour une utilisation
USER MANUAL260-668066-001 JULY 2018 XIavec une antenne parabolique ou à une antenne plate d’un gain maximum de 43 dBi.Se référer à la Antennas certified for use with IRU 600v4 at 5.8GHz on page 125pour une liste d’antennes approuvée pour l’utilisation avec cette radio.lEn vertu des règlements de l'ISED, cet émetteur radio ne peut fonctionner qu'avecune antenne de type et un gain maximum (ou inférieur) approuvé pour l'émetteurpar l'ISED. Pour réduire les interférences radio potentielles avec d'autresutilisateurs, le type d'antenne et son gain doivent être choisis de manière à ce quela puissance isotrope rayonnée équivalente (eirp) ne soit pas supérieure à cellenécessaire à établissement de la liaison.International Use of 5.8 GHzIRU600, 5.8 GHz, does not employ DFS, and as such the equipment cannot be deployed withinEurope or any country where DFS is a regulatory requirement for protection of radars.Networking Devices in Electric Power SubstationsFor IEEE 1613 compliant products, category 7 Ethernet cables must be used in order toensure compliance.NEBS ComplianceThe Eclipse Node comprising the INU/ INUe and IRU 600 complies with the relevant NEBSrequirements under GR-1089-CORE and GR-63-CORE.Such compliance requires installation of the Fan Air Filter option in the INUs, and adherenceto the health and safety and equipment installation practices described herein.WEEE DirectiveIn accordance with the WEEE Directive (2012/19/EU), Eclipse is marked with the followingsymbol:This symbol indicates that this equipment should be collected separately for the purposes ofrecovery and/or recycling.For information about collection and recycling of Aviat Networks equipment please contactyour local Aviat Networks sales office. If you purchased your product via a distributor pleasecontact the distributor for information regarding collection and recovery/recycling.
USER MANUALXII AVIAT NETWORKSMore information on the WEEE Directive is available at our website:http://www.aviatnetworks.com/products/compliance/weee/.(WEEE is the acronym for Waste Electrical and Electronic Equipment)RoHS DirectiveEclipse meets the requirements of ROHS directive 2011/65/EU.Declaration of Conformity, Radio Equipment Directive(RED), 2014/53/EUBulgariaС настоящото Aviat Networks декларира,че този типрадиосъоръжение Eclipse A600/Eclipse A600sp/Eclipse LL/STR 600 ев съответствие с Директива 2014/53/ЕС.Цялостният текст на ЕСдекларацията за съответствие може да се намери на следнияинтернет адрес:www.aviatnetworks.comCzech RepublicTímto Aviat Networks prohlašuje, že typ rádiového zařízení EclipseA600/Eclipse A600sp/Eclipse LL/STR 600 je v souladu se směrnicí2014/53/EU. Úplné znění EU prohlášení o shoděje k dispozici na tétointernetové adrese: www.aviatnetworks.comDenmarkHermed erklærer Aviat Networks, at radioudstyrstypen EclipseA600/Eclipse A600sp/Eclipse LL/STR 600 er i overensstemmelse meddirektiv 2014/53/EU. EU-overensstemmelseserklæringens fulde tekstkan findes på følgende internetadresse: www.aviatnetworks.comGermany Austria Switzerland BelgiumLuxembourg Netherlands LiechtensteinHiermit erklärt Aviat Networks, dass der Funkanlagentyp EclipseA600/Eclipse A600sp/Eclipse LL/STR 600 der Richtlinie 2014/53/EUentspricht. Der vollständige Text der EU-Konformitätserklärung istunter der folgenden Internetadresse verfügbar:www.aviatnetworks.comEstoniaKäesolevaga deklareerib Aviat Networks, et käesolev raadioseadmetüüp Eclipse A600/Eclipse A600sp/Eclipse LL/STR 600 vastab direktiivi2014/53/EL nõuetele. ELi vastavusdeklaratsiooni täielik tekst onkättesaadav järgmisel internetiaadressil: www.aviatnetworks.comUnited Kingdom Ireland MaltaHereby, Aviat Networks declares that the radio equipment type EclipseA600/Eclipse A600sp/Eclipse LL/STR 600 is in compliance withDirective 2014/53/EU. The full text of the EU declaration of conformity isavailable at the following internet address:www.aviatnetworks.comSpainPor la presente, Aviat Networks declara que el tipo de equiporadioeléctrico Eclipse A600/Eclipse A600sp/Eclipse LL/STR 600 esconforme con la Directiva 2014/53/UE. El texto completo de ladeclaración UE de conformidad está disponible en la dirección Internetsiguiente: www.aviatnetworks.com
USER MANUAL260-668066-001 JULY 2018 XIIIGreece CyprusΜε την παρούσα ο/ηAviat Networks, δηλώνει ότι ο ραδιοεξοπλισμόςEclipse A600/Eclipse A600sp/Eclipse LL/STR 600 πληροί την οδηγία2014/53/ΕΕ.Το πλήρες κείμενο της δήλωσης συμμόρφωσης ΕΕδιατίθεται στην ακόλουθη ιστοσελίδα στο διαδίκτυο:www.aviatnetworks.comFrance Luxembourg Switzerland BelgiumLe soussigné, Aviat Networks, déclare que l'équipementradioélectrique du type Eclipse A600/Eclipse A600sp/Eclipse LL/STR600 est conforme à la directive 2014/53/UE. Le texte complet de ladéclaration UE de conformité est disponible à l'adresse internetsuivante: www.aviatnetworks.comItaly SwitzerlandIl fabbricante, Aviat Networks, dichiara che il tipo di apparecchiaturaradio Eclipse A600/Eclipse A600sp/Eclipse LL/STR 600 è conforme alladirettiva 2014/53/UE. Il testo completo della dichiarazione diconformità UE è disponibile al seguente indirizzo Internet:www.aviatnetworks.comLatviaAr šo Aviat Networks deklarē, ka radioiekārta Eclipse A600/EclipseA600sp/Eclipse LL/STR 600 atbilst Direktīvai 2014/53/ES. Pilns ESatbilstības deklarācijas teksts ir pieejams šādāinterneta vietnē:www.aviatnetworks.comLithuaniaAš, Aviat Networks, patvirtinu, kad radijo įrenginiųtipas EclipseA600/Eclipse A600sp/Eclipse LL/STR 600 atitinka Direktyvą2014/53/ES. Visas ES atitikties deklaracijos tekstas prieinamas šiuointerneto adresu: www.aviatnetworks.comNetherlands BelgiumHierbij verklaar ik, Aviat Networks, dat het type radioapparatuurEclipse A600/Eclipse A600sp/Eclipse LL/STR 600 conform is metRichtlijn 2014/53/EU. De volledige tekst van de EU-conformiteitsverklaring kan worden geraadpleegd op het volgendeinternetadres: www.aviatnetworks.comCroatiaAviat Networks ovime izjavljuje da je radijska oprema tipa EclipseA600/Eclipse A600sp/Eclipse LL/STR 600 u skladu s Direktivom2014/53/EU. Cjeloviti tekst EU izjave o sukladnosti dostupan je nasljedećoj internetskoj adresi: www.aviatnetworks.comMaltaB'dan, Aviat Networks, niddikjara li dan it-tip ta' tagħmir tar-radjuEclipse A600/Eclipse A600sp/Eclipse LL/STR 600 huwa konformi mad-Direttiva 2014/53/UE. It-test kollu tad-dikjarazzjoni ta' konformità tal-UE huwa disponibbli f'dan l-indirizz tal-Internet li ġej:www.aviatnetworks.comHungaryAviat Networks igazolja, hogy a Eclipse A600/Eclipse A600sp/EclipseLL/STR 600 típusú rádióberendezés megfelel a 2014/53/EU irányelvnek.Az EU-megfelelőségi nyilatkozat teljes szövege elérhetőa következőinternetes címen: www.aviatnetworks.comPolandAviat Networks niniejszym oświadcza, że typ urządzenia radiowegoEclipse A600/Eclipse A600sp/Eclipse LL/STR 600 jest zgodny zdyrektywą2014/53/UE. Pełny tekst deklaracji zgodności UE jestdostępny pod następującym adresem internetowym:www.aviatnetworks.com
USER MANUALXIV AVIAT NETWORKSPortugalAviat Networks niniejszym oświadcza, że typ urządzenia radiowegoEclipse A600/Eclipse A600sp/Eclipse LL/STR 600 jest zgodny zdyrektywą2014/53/UE. Pełny tekst deklaracji zgodności UE jestdostępny pod następującym adresem internetowym:www.aviatnetworks.comSloveniaAviat Networks potrjuje, da je tip radijske opreme Eclipse A600/EclipseA600sp/Eclipse LL/STR 600 skladen z Direktivo 2014/53/EU. Celotnobesedilo izjave EU o skladnosti je na voljo na naslednjem spletnemnaslovu: www.aviatnetworks.comSlovakiaAviat Networks týmto vyhlasuje, že rádiové zariadenie typu EclipseA600/Eclipse A600sp/Eclipse LL/STR 600 je v súlade so smernicou2014/53/EÚ. Úplné EÚ vyhlásenie o zhode je k dispozícii na tejtointernetovej adrese: www.aviatnetworks.comFinlandAviat Networks vakuuttaa, että radiolaitetyyppi Eclipse A600/EclipseA600sp/Eclipse LL/STR 600 on direktiivin 2014/53/EU mukainen. EU-vaatimustenmukaisuusvakuutuksen täysimittainen teksti on saatavillaseuraavassa internetosoitteessa: www.aviatnetworks.comSwedenHärmed försäkrar Aviat Networks att denna typ av radioutrustningEclipse A600/Eclipse A600sp/Eclipse LL/STR 600 överensstämmer meddirektiv 2014/53/EU. Den fullständiga texten till EU-försäkran omöverensstämmelse finns på följande webbadress:www.aviatnetworks.comIcelandHér með lýsir Aviat Networks yfir því aðEclipse A600/EclipseA600sp/Eclipse LL/STR 600 er í samræmi við grunnkröfur og aðrarkröfur, sem gerðar eru í tilskipun 2014/53/EU.NorwayAviat Networks erklærer herved at utstyret Eclipse A600/EclipseA600sp/Eclipse LL/STR 600 er i samsvar med de grunnleggende krav ogøvrige relevante krav i direktiv 2014/53/EU.RomâniaPrin prezenta, Aviat Networks declarăcătipul de echipamente radioEclipse A600/Eclipse A600sp/Eclipse LL/STR 600 este în conformitatecu Directiva 2014/53/UE. Textul integral al declarației UE deconformitate este disponibil la următoarea adresăinternet:www.aviatnetworks.comFull declarations of conformity are available at:http://aviatnetworks.com/doc/EclipseA600.pdfhttp://aviatnetworks.com/doc/EclipseA600sp.pdfhttp://aviatnetworks.com/doc/EclipseLL.pdfhttp://aviatnetworks.com/doc/STR60011.pdfhttp://aviatnetworks.com/doc/STR600L6U678.pdfCountry Availability MatrixAviat’s radios are classified under the Radio Equipment Directive (2014/53/EU) as Class 2products. For details of where the equipment is intended to be used, see the country matrixbelow.Aviat Networks intends to market this equipment where a cross (X) is shown.
USER MANUAL260-668066-001 JULY 2018 XVBand (GHz) L6 U6 07 08 10 11 13 15 18 23 26 28 32 38 42Austria XXXXXXXXXXXXXXXBelgium XXXX XXXXXXXXXBulgaria XXXXXXX XXXXXXCyprus XXXXXXXXXXXXXXCzech Republic X X X X X X X X X X XDenmark X X X X X X X X X X X XEstonia XXXXXXXXXXXXXXXFinland XXXXX XXXXXXXXXFrance XXXXXXXXXXXXXXGermany XXXXXXXXXXXXXXXGreece X X X X X X X XHungary X X X X X X X X X X XIceland XXXXXXXXXXXX XIreland X X X X X X X X X X XItaly XXXXXXXXXXX XXLatvia X X X X X X X X X X XLithuania XXXXXXXXXXXXXXLuxembourg X X X X X X X X X X X X XMalta XXXXXXXXXX XXXNetherlands X X X X X X X X X X XNorway XXXX XXXXXXX XXPoland XXXX XXXXXXXXXXPortugal X X X X X X X X X X X XRomania XXXXXXXXXXXXXXXSlovak Republic X X X X X X X X X X X X XSlovenia XXXX XXXXXXXXXXSpain XX XXXXXXXXX XSweden X X X X X X X X X X XSwitzerland X X X X X X X X X X X X X XUnited Kingdom X X X X X X X X X X X X XIT SHOULD BE NOTED THAT A LICENSE TO OPERATE THIS EQUIPMENT WILL BEREQUIRED AND THE RELEVANT REGULATOR MUST BE CONTACTED PRIOR TOINSTALLATION AND COMMISSIONING.
USER MANUALXVI AVIAT NETWORKSContentsCopyright & Terms of Use iiiAviat NetworksTechnical Support vProduct Compliance Notes viiRegulatory Information for 5.8 GHz Band viiNetworking Devices in Electric Power Substations xiNEBS Compliance xiWEEE Directive xiRoHS Directive xiiDeclaration of Conformity, Radio Equipment Directive (RED), 2014/53/EU xiiContents xviCHAPTER 1. ABOUT ECLIPSE 19What Is Eclipse? 20Installation and User Prerequisites 21About the Eclipse Documentation 22Conventions and Terminology 23CHAPTER 2. HEALTH AND SAFETY 25General Health and Safety 26Operator Health and Safety 27General Hazards 28RF Exposure Guidelines 32ODU 600 32STR 600 33ODU 300 Series 33Routine Inspection and Maintenance 37Routine Inspections 37Trend Analysis 37Fault Analysis 38Training 38Spares 38CHAPTER 3. SYSTEM OVERVIEW 39Eclipse Node and Packet Node 40Node Indoor Units 41INU 41INUe 42Plug-in Cards 42Plug-in Cards Overview 43Protection Options 53
USER MANUAL260-668066-001 JULY 2018 XVIILink/Path Protection 53Interface Protection 53Network/Data Protection 54Platform Protection 55Eclipse Packet Node and Data Packet Plane 55Data Packet Plane 55Advanced Adaptive Coding and Modulation (ACM) 56Platforms 57Platform Layout 57Slot Assignments 58Eclipse Terminals 60300 Series Indoor Units 60IDU 300 Series Overview 61Eclipse Radio Frequency Units 67IRU 600 67IRU 600 Variants 685.8 GHz Unlicensed Band 74Eclipse Licensing 76Eclipse Configuration and Management 80Eclipse Antennas 81Eclipse Power Supply 82CHAPTER 4. INTRODUCTION TO ECLIPSE INSTALLATION 83Installation Overview 84Before Going On Site 85Installation Tools and Materials 85Unpacking the Eclipse Equipment 86CHAPTER 5. IRU 600 INSTALLATION 87IRU 600 Compatibility 88IRU 600 Installation Procedure 90Chassis Installation 90Chassis Grounding 93NEBS Compliant Grounding 93Safety Requirements for Equipment Grounding 94Waveguide Installation 94Waveguide Connection to ACU 94Power Supply Connection 95Insertion Loss Labels 97Expansion Port Use 97FAN Module 97Chassis Adapter Kit for IRU 600v3 and IRU 600v4 RFUs 98Next Steps 100CHAPTER 6. INSTALLING THE INU AND INUE101INU/INUe Description 102INU Front Panel Layout 102
USER MANUALXVIII AVIAT NETWORKSINU Power Supply 103Power Consumption and INU Load Maximums 103PCC +24 Vdc Operation 111Power Cables 112Fuses 113FAN Air Filter Option 113Fan Air Filter Installation 113Power Line Filter Option 114INU/INUe Installation Requirements 115Installation 118Plug-in Installation Requirements 121APPENDIX A. ANTENNAS CERTIFIED FOR USE WITH IRU600V4AT 5.8GHZ125
ABOUT ECLIPSE CHAPTER 1Chapter 1. About EclipseWelcome to the Eclipse User Manual.This introduction describes:lWhat Is Eclipse? on page 20lInstallation and User Prerequisites on page 21lAbout the Eclipse Documentation on page 22lAbout the Eclipse Documentation on page 22AVIAT NETWORKS JULY 2018 19
CHAPTER 1ABOUT ECLIPSEWhat Is Eclipse?The Eclipse Microwave Radio System comprises the indoor mounted Node or Terminal, andasscociated indoor or outdoor radio frequency units.lEclipse Node supports multiple point-to-point radios for Ethernet, PDH, SDH, on asingle rack-mounted platform, to form a complete network node for star or ringconfigurations on frequency bands 5 to 42 GHz. Plug-in modules provide thecustomization for link and user interface requirements.lEclipse Terminal is optimized for single-link installations or where back-to-backnetwork connection of terminals is preferred. Terminals may also be used onspur links from an Eclipse Node. Different versions are available for Ethernet,PDH, SDH, on frequency bands 5 to 42 GHz.20 JULY 2018 AVIAT NETWORKS
ABOUT ECLIPSE CHAPTER 1Installation and User PrerequisitesTo install, commission, and maintain Eclipse, we recommend you have the followingknowledge and skills:lA basic understanding of the principles of microwave transmission.lInstallation and maintenance experience on Ethernet, PDH and SDH digitalmicrowave radio systems.lFamiliarity with Ethernet and/or SDH multiplexing where these traffic options areto be employed on Eclipse.lFamiliarity with the operation of a PC using the Windows operating system.lA thorough understanding of Eclipse systems, configuration, and diagnosticsfrom attendance of an Aviat Networks training course on Eclipse.WARNING: Follow health and safety procedures at all times! See Health and Safetyon page 25 for complete details.AVIAT NETWORKS JULY 2018 21
CHAPTER 1ABOUT ECLIPSEAbout the Eclipse DocumentationThis documentation provides information on installing, configuring, commissioning, andtroubleshooting an Eclipse Microwave Radio system. Technical descriptions are at amodule and system level.Intended AudienceThis information is for use by trained technicians or engineers. It does not provideinformation or instruction on basic technical procedures. Aviat Networks recommends youread the relevant sections of this manual thoroughly before beginning any installation oroperational procedures.OrganizationThis manual is divided into five volume-level sections:lHealth and Safety RequirementslSystem OverviewlInstallationlConfiguration and DiagnosticslCommissioning and TroubleshootinglAppendicesAdditional ResourcesThe resources identified below contain additional information.lEclipse Platform Product Description. Operational and application data forEclipse Packet Node.lIDU GE3 16x Product Description. Operational and application data forEclipse IDU GE3 16x.lVarious White Papers.lAviat Networks Microwave Radio System Best Practices Guide. (PN 260-668029-001). Use to assist in installing, commissioning, andtroubleshooting Eclipse and other microwave radio products.Contact Aviat Networks or your supplier for availability.22 JULY 2018 AVIAT NETWORKS
ABOUT ECLIPSE CHAPTER 1Conventions and TerminologyThis document uses the following conventions and terminology.Graphic CuesThe following items have graphic cues to identify important supporting information.NOTE: Anote item identifies additional information about a procedure orfunction.CAUTION: Acaution item identifies important information pertaining to actions that maycause damage to equipment, loss of data, or corruption of files.WARNING: Awarning item identifies a serious physical danger or major possibleproblem.Font ChangesBold font is used for the names of on-screen elements such as; fields, buttons, and drop-down selection lists, keywords, commands and for keys on the keyboard.Courier font in blue text is used to indicate commands that the user needs to type in.WTM4100# show radio-carrier status Carrier1/1Any responses or report output from a command is shown as brown text and indented.radio-carrier status Carrier1/1oper-status upItalic font is used to emphasize words and phrases, to introduce new terms, and for thetitles of printed publications.Common TerminologyClick or Select: Point the mouse pointer at the item you want to select, then quickly press andrelease the left mouse button.Right-Click: Point the mouse pointer at the item you want to select, then quickly press andrelease the right mouse button.AVIAT NETWORKS JULY 2018 23
HEALTH AND SAFETY CHAPTER 2Chapter 2. Health and SafetyThis section includes the following health and safety information:lGeneral Health and Safety on page 26lOperator Health and Safety on page 27lGeneral Hazards on page 28lRF Exposure Guidelines on page 32All personnel must comply with the relevant health and safety practices when working on oraround Eclipse radio equipment.The Eclipse system has been designed to meet relevant US and European health and safetystandards as outlined in IEC Publication 60950-1.Eclipse is a Class A product. It is intended to be used exclusively in telecommunicationscenters.Local safety regulations must be used if mandatory. Safety instructions in this Volumeshould be used in addition to the local safety regulations. In the case of conflict betweensafety instructions stated herein and those indicated in local regulations, mandatory localnorms will prevail. Should not local regulations be mandatory, then safety norms hereinwill prevail.WARNING: Hot Surfaces - the external surfaces of an ODU 600v2 can be hot to touch,especially at high ambient temperatures. A hot surfaces warning icon is displayed onthe product:AVIAT NETWORKS JULY 2018 25
CHAPTER 2HEALTH AND SAFETYGeneral Health and SafetyThis table describes general health and safety information about the Eclipse radio.Topic InformationFlammability Eclipse is designed and constructed to minimize the risk of smoke and fumes duringa fire.HazardousMaterialsNo hazardous materials are used in the construction of the equipment.HazardousVoltageEclipse meets global product safety requirements for safety extra-low voltage (SELV)rated equipment where the input voltage must be 48V nominal, 60V maximum.Safety Signs External warning signs or other indicators on the equipment are not required.SurfaceTemperaturesThe external equipment surfaces do become warm during operation due to heatdissipation. However, the temperatures reached are not considered hazardous.26 JULY 2018 AVIAT NETWORKS
HEALTH AND SAFETY CHAPTER 2Operator Health and SafetyThe following table describes the precautions that relate to installing or working on anEclipse radio.Topic InformationEquipmentProtrusionsEclipse has been designed to be free of unnecessary protrusions or sharp surfacesthat may catch or otherwise cause injury during handling. However, always takecare when working on or around the equipment.Laser and FiberOptic Cable HazardsEclipse fiber optic transmitters are IEC60825-1 / 21CFR1040-1 Class I compliantand present no danger to personnel in normal use. However:Do not look into active unterminated optical ports or fibers. If visual inspection isrequired ensure the equipment is turned off or, if a fiber cable, disconnect the farend.Follow the manufacturer's instructions when using an optical test set. Incorrectcalibration or control settings could result in hazardous levels of radiation.Protect/cover unconnected optical fiber connectors with dust caps.Place all optical fiber cuttings in a suitable container for safe disposal. Bare fibersand fiber scraps can easily penetrate the skin and eyes.Lifting Equipment Be careful when hoisting or lifting an antenna or ODU during installation ormaintenance. A large antenna with its mounting hardware can weigh in excess of100kg (220 lb) and require specialized lifting equipment and an operator trainedand certified in its use.Protection from RFExposure: EclipseEclipse radio transceivers do not generate RF fields intense enough to cause RFburns. However, when installing, servicing or inspecting an antenna always complywith the Protection from RF Exposure guidelines under General Hazards onpage 28.Safety Warnings When a practice or procedure poses implied or potential harm to the user or to theEclipse equipment, a warning is included in this manual.AVIAT NETWORKS JULY 2018 27
CHAPTER 2HEALTH AND SAFETYGeneral HazardsThe following table describes the general hazards that must be addressed when planningand installing an Eclipse system.For more information on health and safety when using Aviat Networks products, refer to theBest Practices Guide.Topic InformationAirflow Requirements Rack installations must be made so the airflow required for safe and correctoperation of Eclipse is not compromised. For the fan-cooled Eclipse INUsand fan-cooled Eclipse IDUs, unobstructed air passage must be maintainedto each side of the chassis, which requires a minimum of 50 mm (2 inches)of side spacing to any rack panels, cable bundles or similar. Unused slots onthe INU/INUe must be fitted with a blanking panel.Where a Fan Air Filter is installed in an INU it must not be allowed tobecome clogged with dust. Replace when necessary.Inspection must be atnot more than 12 monthly intervals when installed in telecommunicationsequipment room controlled-air environments. Otherwise, inspection isrequired at more frequent intervals.EMC Eclipse has been tested for and meets EMC Directive 89/336/EEC. Theequipment was tested using screened cable; if any other type of cable isused, it may violate compliance.Eclipse is a Class A product. In a domestic environment this product maycause radio interference in which case the user may be required to takeadequate measures. This equipment is intended to be used exclusively intelecommunications centers.ESD ESD (electrostatic discharge) can damage electronic components. Even ifcomponents remain functional, ESD can cause latent damage that results inpremature failure. Always wear proper ESD grounding straps whenchanging or handling the plug-in cards and avoid hand contact with thePCB back-plane and top-plane. Connect your ESD grounding strap to thecombined ESD and ground connector on the INU rack ear. Spare plug-incards or cards to be returned for service must be enclosed in an anti-staticbag. When removing a card from the anti-static bag for installation in anINU, or placing a card in a bag, do so at the INU and only when connected tothe INU via your ESD grounding strap.Circuit Overloading When connecting an Eclipse terminal, determine the effect this will have onthe power supply circuit protection devices, and supply wiring. CheckEclipse power consumption specifications and the supply capability of thepower supply system. This check of capacity must extend to the dc powersupply and not just to an intermediate connection point.28 JULY 2018 AVIAT NETWORKS
HEALTH AND SAFETY CHAPTER 2Topic InformationEclipse Indoor Unit andDC Supply GroundingThe ground for Eclipse indoor unit(s) must be connected directly to the dcsupply system ground conductor, or to a bonding jumper from a groundingterminal bar, or bus to which the dc supply system grounding is connected.Intrabuilding interfacesand cabling for NEBScomplianceIntrabuilding connections to/from Eclipse ports must only be connected viaintrabuilding or unexposed wiring or cabling.Intrabuilding ports MUST NOT be metallically connected to interfaces thatconnect to the OSP or its wiring. These interfaces are designed for use asintrabuilding interfaces only (Type 2 or Type 4 ports as described in GR-1089-CORE, Issue 4) and require isolation from the exposed OSP cabling.The addition of Primary Protectors is not sufficient protection in order toconnect these interfaces metallically to OSP wiring.Shielded and grounded cables must be used for intrabuilding cablingto/from Eclipse ports. Cables must be grounded at both ends.Protection from RFExposureWhen installing, servicing or inspecting an antenna always comply with thefollowing:Locate the antenna such that it does not infringe the RF exposureguidelines for general public. Refer to General Public ComplianceBoundary in RF Exposure Guidelines on page 32.Stay aware of the potential risk of RF exposure and take appropriateprecautions. Refer to Occupational Compliance Boundary in RFExposure Guidelines on page 32.Do not stand in front of or look into an antenna without first ensuring theassociated transmitter or transmitters are switched off.Do not look into waveguide or into the waveguide port of an RFU withoutfirst ensuring the associated transmitter or transmitters are switched off.At a multi-antenna site ask the site owner or operator for details of otherradio services active at the site and for theirrequirements/recommendations for protection against potentiallyharmful exposure to RF radiation.When it is not possible to switch transmitters off at a multi-antenna siteand there is potential for exposure to harmful levels of RF radiation, weara protective suit.Fiber Optic Cables Handle optical fibers with care. Keep them in a safe and secure locationduring installation.Do not attempt to bend them beyond their minimum bend radius.Protect/cover unconnected optical fiber connectors with dust caps.Ground Connections Reliable grounding of the Eclipse system must be maintained. Refer toinstructions in the manual for grounding of waveguide, ODU cable, lightningsurge suppressor, ODU, and indoor unit.There must be no switching or disconnecting devices fitted in groundconductors.Lightning SurgeSuppressorEclipse ODU cables must be fitted with the specified surge suppressor atthe ODU unless the ODU has a built-in suppressor.AVIAT NETWORKS JULY 2018 29
CHAPTER 2HEALTH AND SAFETYTopic InformationMains Power SupplyRoutingEclipse dc power, IF, tributary, auxiliary and NMS cables are not to be routedwith any AC mains power lines. They are also to be kept away from anypower lines which cross them.Maximum AmbientTemperatureThe maximum ambient temperature (Tmra) for Eclipse indoor units andoutdoor units is +55° C (131° F). Special conditions apply to the INUs - formore information see Power Consumption within INU Power Supply onpage 103. To ensure correct operation and to maximize long termcomponent reliability, ambient temperatures must not be exceeded.Operational specification compliance is not guaranteed for higher ambients.Mechanical Loading When installing an indoor unit in a rack, ensure the rack is securelyanchored. Ensure that the additional loading of an Eclipse indoor unit orunits will not cause any reduction in the mechanical stability of the rack.Power SupplyConnectionThe Eclipse INU/INUe and IDUs have the +ve pin on their dc power supplyconnector connected to chassis ground. It must be used with a-48Vdc power supply which has a +ve ground; the power supply groundconductor is the +ve supply to the radio. For NEBS compliance the batteryreturn connection is to be treated as a common DC return (DC-C), as definedin GR-1089-CORE.For IRU 600 variants that require a separate wide-mouth +/-21 to+/-60 Vdc power supply connection, both pins on its power supply connectorare isolated from chassis ground. For NEBS compliance the battery returnconnection is to be treated as an isolated DC return (DC-I), as defined in GR-1089-CORE.The d.c. supply source must be located within the same premises as theequipment.Connection to D.C. SupplyGroundCAUTION: The Eclipse INU/INUe and IDUs have a connectionbetween the earthed conductor of the d.c. supply circuit and theearthing conductor.This equipment must be connected directly to the d.c. supply systemgrounding electrode conductor or to a bonding jumper from a groundingterminal bar or bus to which the d.c. supply system grounding electrode isconnected.Switching or disconnecting devices must not be in the grounded circuitconductor between the d.c. source and the point of connection of thegrounding electrode conductor.This equipment must be located in the same immediate area (such as,adjacent cabinets) as any other equipment that has a connection betweenthe grounded conductor of the same d.c. supply circuit and the groundingconductor, and also the point of grounding of the d.c. system. The d.c.system shall not be grounded elsewhere.Power SupplyDisconnectAn appropriate disconnect device for the -48 Vdc or +24 Vdc power supplyunit must be provided as part of the building installation.30 JULY 2018 AVIAT NETWORKS
HEALTH AND SAFETY CHAPTER 2Topic InformationRack Mount TemperatureConsiderationsIf the Eclipse indoor unit is installed in a closed or multi-unit rack assembly,the operating ambient temperature of the rack environment may be greaterthan room ambient. The maximum ambient temperature applies to theimmediate operating environment of the Eclipse indoor unit, which, ifinstalled in a rack, is the ambient within the rack.Restricted Access The Eclipse system must be installed in restricted access sites. The indoorunit and associated power supply must be installed in restricted areas, suchas dedicated equipment rooms, closets, cabinets, or the like. Access to thetower and antenna location must be restrictedNOTE: F or U S A:In restric ted acc ess areas install the E clips e s ys tem in ac c ordance witharticles 110-26 and 110-27 of the 2002 National Elec tric al CodeANSI/NFPA 70, or to any subs equent update to this c ode for the rel evantarticles.AVIAT NETWORKS JULY 2018 31
CHAPTER 2HEALTH AND SAFETYRF Exposure GuidelinesData is provided for Eclipse ODU 600, STR 600 and ODU 300.ODU 600The following MPE (maximum permissible exposure) calculations have been produced inaccordance with the guidelines of EN 50383/EN 50385 and Section 1.1310 of the FCC’srules. These calculations represent the maximum conducted output power and themaximum antenna gain, by frequency range. These calculations are based on the exposurerequirements for the general public. If the antennas used with this device exceed the gainvalues stated below, the installer must take additional precautions and re-calculate theminimum compliance boundary.Table 1. MPE Guidelines for ODU 600Frequency Range(GHz)Minimum Com-pliance Distance(m)TX conductedpower (dBm)Antenna Gain(dBi)4.4 – 5.0 15.86 +30.0 45.05.925 - 7.11 9.78 +31 39.87.125 – 7.9 12.75 +32 41.17.725 - 8.5 11.36 +31 41.110.7 – 11.7 10.48 +27 44.412.75 – 13.25 11.23 +26.5 45.514.4 – 15.35 12.61 +26.5 46.517.7 – 19.7 10.49 +23 48.421.2 - 23.632 13.2 +23.5 49.924.25 – 26.483 12.31 +25 47.827.5 – 29.5 7.09 +25 43.031.8 – 33.4 6.18 +23 43.837.0 – 39.46 7.78 +23 45.840.5 - 43.5 6.54 +21 46.3Operation of ODU 600 on 5.8 GHz Unlicensed Band, USA and CanadaTo ensure compliance with FCC and Industry Canada RF exposure requirements, aminimum distance of 18 meters must be maintained between the ODU 600 antenna and anypersons whilst the unit is operational. This calculation is based on the maximum conductedpower and maximum antenna gain permitted by FCC and Industry Canada RF for this band.32 JULY 2018 AVIAT NETWORKS
HEALTH AND SAFETY CHAPTER 2STR 600The following MPE (maximum permissible exposure) calculations have been produced inaccordance with the guidelines of EN 50383/EN 50385 and Section 1.1310 of the FCC’srules. These calculations represent the maximum conducted output power and themaximum antenna gain, by frequency range. These calculations are based on the exposurerequirements for the general public. If the antennas used with this device exceed the gainvalues stated below, the installer must take additional precautions and re-calculate theminimum compliance boundary.Table 2. MPE Guidelines for STR 600Frequency Range(GHz)Minimum Com-pliance Distance(m)TX conductedpower (dBm)Antenna Gain(dBi)4.4 – 5.0 17.80 +31.0 45.05.925 - 7.11 13.04 +33.5 39.87.125 – 7.9 15.15 +33.5 41.17.725 -8.5 13.50 +32.5 41.110.0 – 11.7 15.69 +30.5 44.4ODU 300 SeriesThe following MPE (maximum permissible exposure) calculations for the Eclipse ODU 300series have been produced in accordance with the guidelines of EN 50383/EN 50385. Thesecalculations represent examples only and do not include every possible combination ofoutput power and antenna gain.Occupational is defined as: “The occupationally exposed population consists of adults whoare generally exposed under known conditions and are trained to be aware of potential riskand to take appropriate precautions”.Table 3. MPE Guidelines for ODU 3005 GHz (4.4 - 5.0 GHz)Transmit Power(dBm)Antenna Gain (dBm) Compliance BoundaryGeneral Public (m)Compliance BoundaryOccupational (m)30.5 39.3 8.77 3.9130.5 32.6 4.06 1.810.5 39.3 0.28 0.120.5 32.6 0.13 0.06L6/U6 GHz (5.925 - 7.11 GHz)AVIAT NETWORKS JULY 2018 33
CHAPTER 2HEALTH AND SAFETYTransmit Power(dBm)Antenna Gain (dBm) Compliance BoundaryGeneral Public (m)Compliance BoundaryOccupational (m)30.5 41.5 11.30 5.0330.5 31.2 3.45 1.540.5 41.5 0.36 0.160.5 31.2 0.11 0.057/8 GHz (7.125 - 8.5 GHz)Transmit Power(dBm)Antenna Gain (dBm) Compliance BoundaryGeneral Public (m)Compliance BoundaryOccupational (m)30.5 42.9 13.28 5.9130.5 30.24 3.15 1.405.0 42.9 0.71 0.315.0 30.4 0.17 0.0710 GHz (10.0 - 10.68 GHz)Transmit Power(dBm)Antenna Gain (dBm) Compliance BoundaryGeneral Public (m)Compliance BoundaryOccupational (m)26.0 34.3 2.94 1.3126.0 33.7 2.74 1.22-4.0 34.3 0.09 0.04-4.0 33.7 0.09 0.0411 GHz (10.7 - 11.7 GHz)Transmit Power(dBm)Antenna Gain (dBm) Compliance BoundaryGeneral Public (m)Compliance BoundaryOccupational (m)25.0 46.2 10.31 4.5925.0 27.7 1.23 0.552.5 46.2 0.77 0.342.5 27.7 0.09 0.0413 GHz (12.75- 13.25 GHz)Transmit Power(dBm)Antenna Gain (dBm) Compliance BoundaryGeneral Public (m)Compliance BoundaryOccupational (m)28.0 47.3 16.53 7.3628.0 29.6 2.15 0.960.0 47.3 0.66 0.290.00 47.3 0.66 0.290.00 29.6 0.09 0.0415 GHz (14.4- 15.35 GHz)Transmit Power(dBm)Antenna Gain (dBm) Compliance BoundaryGeneral Public (m)Compliance BoundaryOccupational (m)34 JULY 2018 AVIAT NETWORKS
HEALTH AND SAFETY CHAPTER 227.0 46.4 13.28 5.9127.0 30.8 2.20 0.98-1.0 46.4 0.53 0.24-1.0 30.8 0.09 0.0418 GHz (17.7-19.7 GHz)Transmit Power(dBm)Antenna Gain (dBm) Compliance BoundaryGeneral Public (m)Compliance BoundaryOccupational (m)21.5 48.0 8.48 3.7721.5 32.8 1.47 0.66-3.0 48.0 0.50 0.22-3.0 32.8 0.09 0.0423 GHz (21.2-23.632 GHz)Transmit Power(dBm)Antenna Gain (dBm) Compliance BoundaryGeneral Public (m)Compliance BoundaryOccupational (m)21.5 49.2 9.73 4.3321.5 34.4 1.77 0.79-3.0 49.2 0.58 0.26-3.0 34.4 0.11 0.0526 GHz (24.52- 26.483 GHz)Transmit Power(dBm)Antenna Gain (dBm) Compliance BoundaryGeneral Public (m)Compliance BoundaryOccupational (m)15.5 46.0 3.37 1.5015.5 35.9 1.05 0.47-4.5 46.0 0.34 0.15-4.5 35.9 0.11 0.0528 GHz (27.5- 29.5GHz)Transmit Power(dBm)Antenna Gain (dBm) Compliance BoundaryGeneral Public (m)Compliance BoundaryOccupational (m)15.0 48.1 4.06 1.8115.0 36.5 1.07 0.48-5.0 48.1 0.41 0.18-5.0 36.5 0.11 0.0532 GHz (31.8- 33.4 GHz)Transmit Power(dBm)Antenna Gain (dBm) Compliance BoundaryGeneral Public (m)Compliance BoundaryOccupational (m)17.5 43.5 3.19 1.4217.5 37.5 1.60 0.71AVIAT NETWORKS JULY 2018 35
CHAPTER 2HEALTH AND SAFETY-5.0 43.5 0.24 0.11-5.0 37.5 0.12 0.0538 GHz (37.0- 39.46 GHz)Transmit Power(dBm)Antenna Gain (dBm) Compliance BoundaryGeneral Public (m)Compliance BoundaryOccupational (m)17.5 48.1 5.41 2.4117.5 39.3 1.96 0.87-5.0 48.1 0.41 0.18-5.0 39.3 0.15 0.0736 JULY 2018 AVIAT NETWORKS
HEALTH AND SAFETY CHAPTER 2Routine Inspection and MaintenanceThis section overviews required and recommended inspection and maintenance practices toensure health and safety of installed equipment is maintained to highest levels. For moreinformation, refer to the Aviat Networks publication: Best Practices.Routine InspectionsAll sites must be inspected annually, or more frequently if subject to abnormal operatingconditions such as particularly exposed sites, or sites subject to salt-spray or heavysnow/ice loading over winter months.The inspection should cover the physical installation including the antenna, antenna feederor IDU/ODU cable, cable grounding, equipment grounding, tower and building grounds,weatherproofing, lightning surge suppressors, and general site integrity.Where a Fan Air Filter is installed in an INU (for NEBS compliance) it must be inspectedannually, or more frequently if the INU is installed in an environment that is not controlledfor dust exclusion.Selected ground wires should be resistance checked and then compared with previouschecks to ensure there has been no significant change.The operational performance of the radio and associated equipment should be checkedagainst their as-built figures using the Portal or ProVision alarm and performanceindicators.Trend AnalysisUse available current and historical Eclipse alarm and performance data to determine anytrend that may lead to a failure - if allowed to continue.Check for the following trends:lReducing receive signal levelslGradually increasing bit errors or an increasing errored seconds countlChanges in transmit powerlIncreased frequency of rain fade or other fade conditionslIncreasing occurrence of other weather related changes in performancelIncreasing occurrence of a particular hardware failureTime spent in conducting such analysis is time well spent. Catching a problem before itbrings down the network is good network management.AVIAT NETWORKS JULY 2018 37
CHAPTER 2HEALTH AND SAFETYFault AnalysisAll faults, once cleared, should be the subject of a fault report. The data presented in thesereports should be analyzed from time to time to check for any common threads, which maypoint to a particular weakness in the design, installation, or maintenance of the network orto a specific component.The time taken to restore service and the parts used should also be analyzed to see ifimprovements are possible in the maintenance procedures, maintenance training andspares holdings.TrainingProperly trained and experienced planning and installation personnel are essential forestablishing and maintaining high integrity in a new network. Similarly, properly trainednetwork management and service personnel are essential for the continued good health of anetwork.The training needs for personnel should be reviewed from time-to-time to ensure theymaintain expertise in their area of work, and on the installed base.SparesSpares holdings should be reviewed on a regular basis to ensure the correct quantity andtype are held, and held at the most appropriate locations.Analysis of spares usage will show any trend for excessive use of spares, which may pointto a weakness in the deployment or manufacture of the item.Spares holdings should also be checked from time to time and if necessary brought up tothe current hardware and/or software revision level.38 JULY 2018 AVIAT NETWORKS
SYSTEM OVERVIEW CHAPTER 3Chapter 3. System OverviewEclipse is available on two platform types, Node, and Terminal.This section overviews their features and capabilities. Refer to:lEclipse Node and Packet Node on page 40lEclipse Terminals on page 60lEclipse Radio Frequency Units on page 67lEclipse Licensing on page 76lEclipse Strong Security on page 1lEclipse Configuration and Management on page 80lEclipse Antennas on page 81lEclipse Power Supply on page 82AVIAT NETWORKS JULY 2018 39
CHAPTER 3SYSTEM OVERVIEWEclipse Node and Packet NodeEclipse Node supports multiple radio links from a common indoor unit with airlinkthroughput capacities to 366 Mbit/s Ethernet, 100xE1, 127xDS1, 4xDS3, STM1+1E1, or2xSTM1/OC3.Eclipse Packet Node adds a data packet plane (DPP) to support Gigabit Ethernetthroughputs, plus the traffic and capacity options provided on Eclipse Node.Both Eclipse Node and Packet Node use common rack-mounted indoor units, the INU andINUe, and either ODUs for split-mount operation, or an IRU 600 for all-indoor operation.Operation on licensed bands extends from 4 to 38 GHz. Operation on the license-free 5.8GHz ISM band is supported for North America and Canada.Path, equipment, and data protection options support comprehensive link, network and dataredundancy.Plug-in cards on the INU and INUe provide a wide choice of user interfaces and linkoperation. Options include:lIP/EthernetlSynchronous EthernetlE1/DS1lE3/DS3lSTM1/OC3lFixed or adaptive modulationlHot-standby, space diversity, frequency diversity, dual diversitylCCDP/XPIC (co-channel dual polarized with cross-pol interference cancellation)The node-based concept eliminates most ancillary equipment and external cabling, andoffers smooth upgrade paths for next generation networks.Operation is supported by Portal and ProVision. Portal is a PC-based craft tool, ProVision isthe element management system (EMS).See:lNode Indoor Units on page 41lPlug-in Cards on page 42lProtection OptionslEclipse Packet Node and Data Packet Plane on page 55lPlatforms on page 5740 JULY 2018 AVIAT NETWORKS
SYSTEM OVERVIEW CHAPTER 3Figure 1. INUe with High-Power 3RU IRU 600MEF Certified. Eclipse Node and Packet Node meet MEF 9 and MEF 14 requirements forcarrier-class Ethernet inter-operability and performance.lMEF 9 specifies the User Network Interface (UNI)lMEF 14 specifies Quality of Service (QoS)Aviat Networks is ISO90001:2008 and TL9000 Certified. Full certification means alldepartments and business units within Aviat Networks have been strictly assessed forcompliance to both standards. It testifies that Aviat Networks is a certified supplier ofproducts, services and solutions to the highest ISO and Telecommunication standardsavailable.Node Indoor UnitsThere are two indoor units, the INU, and INUe (extended INU). The INU is a 1RU chassis, theINUe 2RU chassis.Mandatory plug-ins are the NCC (Node Control Card) and FAN (Fan card). The optional plug-ins include RAC (Radio Access Card), DAC (Digital Access Card), AUX (Auxiliary), NPC (NodeProtection Card), and PCC (Power Converter Card).INUThe INU requires one NCC and one FAN, and has provision for four option plug-ins. Itsupports a maximum of three RFUs for three non-protected links, or oneprotected/diversity link and one non-protected link.AVIAT NETWORKS JULY 2018 41
CHAPTER 3SYSTEM OVERVIEWFigure 2. INUINUeThe INUe requires one NCC and one 2RU FAN, and has provision for ten option cards. Itsupports a maximum of six RFUs for six non-protected links, or up to threeprotected/diversity links.Figure 3. INUePlug-in CardsPlug-in cards for the INU or INUe enable quick and easy customization on Eclipseconfigurations. All cards are hot-pluggable.RACs support the radio modem function. In the transmit direction they take the digital trafficfrom the backplane or data packet plane and convert it to an IF signal for connection to anRFU (ODU or IRU 600). The reverse occurs in the receive direction.lOne RAC/ODU or RAC/IRU 600 combination is used for a 1+0 link.lTwo RAC/ODUs or two RACs with one 1+1 IRU 600 are used for 1+1 hot-standbyor diversity links.lRACs control TX switching and RX voting on protected / diversity links. DifferentRACs support different capacity and modulation options.42 JULY 2018 AVIAT NETWORKS
SYSTEM OVERVIEW CHAPTER 3lXPIC (cross polarization interference cancellation) RACs support CCDP (co-channel dual polarization) operation.DACs support the user interface.lDifferent DACs support Ethernet, E1/DS1, E3/DS3, and STM1/OC3 connections.lMultiplexer DACs support transport of STM1/OC3 or E3/DS3 with NxE1/DS1rates.lEthernet DACs support a L2 switch function. DAC GE3 supports advanced optionsfor Synchronous Ethernet, ring/mesh protection, QoS, buffer management, linkaggregation, VLAN tagging, and OAM.lMost DACs can be protected using a stacked (paired) configuration.lE1/DS1, DS3, and STM1/OC3 DACs support Ethernet-over-TDM options to enableEthernet transport over legacy TDM radio or leased-line links.NCM (Network Convergence Module) provides an E1/DS1 loopswitch capability.AUX (Auxiliary card) supports async or sync service-channel connections, and alarm I/Ooptions for connection to external devices.NCC (Node Controller Card) provides Node management and DC-DC converter functions.NCC is a mandatory card.lIt manages Node operation and event collection and management.lIt incorporates a router function for local and remote network managementinterconnection.lNode configuration and licensing data is held in flash-memory.lPower supply: -48 Vdc (SELV -40.5 to -60 Vdc).FAN (Fan card) provides forced-air cooling. FAN is a mandatory card.NPC (Node Protection Card) provides 1+1 protection functions for the NCC power supply andbackplane management.PCC (Power Conversion Card) supports operation from a +24 Vdc power supply.The figure below illustrates the nodal concept and the wide range of plug-in cards.See Plug-in Cards Overview on page 43 for an introduction to the cards and their functions.Plug-in Cards OverviewNOTE: RAC 60, RAC 6X, RAC 3X, RAC 30A, RAC 40, RAC 4X, DAC GE, DACES, DAC 16x are legacy plug-ins - they are no longer manufactured.NOTE: For more detailed information on plug-ins refer to the EclipsePlatform Product Description.AVIAT NETWORKS JULY 2018 43
CHAPTER 3SYSTEM OVERVIEWRAC 70RAC 70 supports DPP (Data Packet Plane) and ACM (Adaptive Coding and Modulation)options. RAC 70 additionally supports airlink recovered timing (ART) for high accuracy radiotransport of a SyncE clock.There are ten dynamically switched modulation rates; QPSK, 16 QAM, 32 QAM, 64 QAM, 128QAM, 256 QAM, 512 QAM, 1024 QAM, 2048 QAM and 4096 QAM, (2048 QAM and 4096 QAMare only available with the ODU 600v2 or IRU 600v4).lAll of the modulation states offered with ACM can be selected for use.lModulation switching (state change) is errorless for priority traffic.A DPP port enables direct routing of Ethernet traffic to a DAC GE3.Payload encryption is a licensed option (this is the same license as for the RAC60/6x/60E/6xE).Individual ACM modulations can be set as fixed rates. These are complemented by fixed-only rates for TDM capacities (DS1). DS3 and OC3 are not supported by the RAC 70.Channel bandwidths range from 10 to 80 MHz ANSI. Air-link capacities for Ethernet, or forEthernet+TDM, extend to 715 Mbit/s. TDM options extend to 127xDS1.ART operation is designed to meet G.8262 synchronization mask requirements for SyncEclock transport.RAC 70 interfaces to an ODU 600, or to the IRU 600.Figure 4. RAC 70RAC7XRAC 7X adds CCDP operation to RAC 70 capabilities.Two RAC 7X cards are operated as a CCDP pair, either in the same INU, or in separate co-located INUs to provide double the capacity over one channel, using both the horizontal andvertical polarizations. An XPIC function between the RACs ensures cross-polarizationinterference is eliminated.44 JULY 2018 AVIAT NETWORKS
SYSTEM OVERVIEW CHAPTER 3Figure 5. RAC 7XRAC 60 and RAC 60ERAC 60 supports DPP (Data Packet Plane) and ACM (Adaptive Coding and Modulation)options. RAC 60E additionally supports airlink recovered timing (ART) for high accuracyradio transport of a SyncE clock.There are four dynamically switched modulation rates; QPSK, 16 QAM, 64 QAM, 256 QAM.Coding options additionally apply on each of these modulations, one for maximumthroughput, one for maximum gain, to provide an effective total of eight modulation states.lMaximum throughput delivers maximum data throughput - at the expense of somesystem gain.lMaximum gain delivers best system gain - at the expense of some throughput.lUp to four of the eight modulation states offered with ACM can be selected for use.lModulation switching (state change) is errorless for priority traffic.A DPP port enables direct routing of Ethernet traffic to a DAC GE/GE3.Individual ACM modulations can be set as fixed rates. These are complemented by fixed-only rates for TDM capacities (E1/DS1, DS3, STM1/OC3) .Channel bandwidths range from 5 to 56 MHz ETSI, and 3.5 to 80 MHz ANSI.Air-link capacities for Ethernet, or for Ethernet+TDM, extend to 366 Mbit/s.TDM options extend to 100xE1, 127xDS1, 4xDS3, 2xSTM1/OC3.Payload encryption is a licensed option.RAC 60E ART operation is designed to meet G.8262 synchronization mask requirements forSyncE clock transport.RAC 60/60E interfaces to an ODU 600, ODU 300hp, or to the IRU 600.A RAC 60 can link to a RAC 6X in non-CCDP mode, or to a RAC 6XE in non-CCDP, non ARTmodes.Figure 6. RAC 60AVIAT NETWORKS JULY 2018 45
CHAPTER 3SYSTEM OVERVIEWRAC 6X and RAC 6XERAC 6X/6XE adds CCDP operation to RAC 60/60E capabilities. RAC 6XE additionally supportsART.Two RAC 6X/6XE cards are operated as a CCDP pair, either in the same INU, or in separateco-located INUs to provide double the capacity over one channel, using both the horizontaland vertical polarizations. An XPIC function between the RACs ensures cross-polarizationinterference is eliminated.A RAC 6X can link to a RAC 6XE where ART capability is not required.Figure 7. RAC 6XEDAC GE3DAC GE3 capabilities include Synchronous Ethernet, link aggregation, policing, ring/meshprotection and Ethernet service OAM.lThree RJ-45 10/100/1000Base-T portslTwo multi-purpose SFP ports with plug-ins for:oOptical LC, 1000Base-LX, 1310 nm single-modeoOptical LC, 1000Base-SX, 850 nm multi-modeoElectrical RJ-45 10/100/1000Base-TlSix transport channel (TC) portslComprehensive QoS traffic prioritization and scheduling options:o802.1p mappingoDiffServ mapping (IPv4, IPv6)oMPLS Exp bits mappingoStrict priority schedulingoDeficit Weighted-Round-Robin (DWRR) schedulingoHybrid strict + DWRR schedulingoEight transmission queueslTraffic policing using TrTCM (two rate, three color metering) with remarkingoptionslL2 LAG (IEEE 802.1AX), static and LACPlL1LA (Layer 1 link aggregation)lAdvanced options for VLAN tagging, including Q (802.1Q), QinQ (802.1ad),Filtering, Translation46 JULY 2018 AVIAT NETWORKS
SYSTEM OVERVIEW CHAPTER 3lSynchronous Ethernet with Stratum 3 hold-over performance on timingsubsystemlRSTP (IEEE 802.1w)lERP (ITU-T 8032v2)lEthernet service OAM (IEEE 802.1ag/IYU-T Y.1731: ETH-CC, ETH-LB, ETH-LT)lData packet plane (DPP) and/or backplane traffic interconnection to RACslAdvanced traffic shaping for fixed and adaptive modulation linkslSuperior burst management with 1500 Kbytes shared memory across activeportslStorm controllJumbo frames to 10 Kbytes bi-directionallFlow control (IEEE 802.3x)l1+1 port and card protectionlInter-frame gap (IFG) and preamble stripping and re-insertionlRMON stats per port, channel, and queuelCompatibility with DAC GE, DAC ES, IDU ES, IDU GE 20x, IDU GE3 16xFigure 8. DAC GE3For DPP traffic a DAC GE3 must be operated with a RAC 70/7X, RAC 60/60E or RAC 6X/6XE.RAC 60E/6XE/70/7X is required for Synchronous Ethernet links.DAC GEDAC GE interfaces three 10/100/1000Base-T electrical ports and one 1000Base-LX opticalport, to one or two transport channels. Features include:lTraffic prioritization optionso802.1p mappingoDiffServ mapping (IPv4)oFour transmission queueslTransparent, VLAN and mixed modes of operationlEnhanced, fast-switched RSTPlLayer 1 or Layer 2 link aggregationlVLAN tagging, for Q and QinQlDPP and backplane traffic connectionslInter-frame gap (IFG) and preamble stripping and re-insertionlFrame sizes to 9600 byteslAssignment to radio or fiber linksAVIAT NETWORKS JULY 2018 47
CHAPTER 3SYSTEM OVERVIEWlSFP optical port options for 1310nm single-mode, or 850nm multi-modelCompatibility with DAC GE3, DAC ES, IDU ES, IDU GE 20x, IDU GE3 16xFigure 9. DAC GEFor DPP traffic a DAC GE must be operated with a RAC 60/60E or RAC 6X/6XE.DAC ESDAC ES interfaces four 10/100Base-T Ethernet ports to one or two radio and/or fibertransport channels. Features include:lAdvanced QoS settingslTransparent, VLAN and mixed modes of operation.lThroughputs to 100 Mbit/s per transport channellAssignment to radio or fiber linkslInter-frame gap (IFG) and preamble stripping and re-insertionlCompatibility with DAC GE3, DAC GE, IDU ES, IDU GE 20x, IDU GE3 16xFigure 10. DAC ESDAC 16XDAC 16x supports 16xE1 or 16xDS1 tributaries on Mini RJ-21 connectors.Figure 11. DAC 16xDAC 16xV2/V3DAC 16xV2/V3 supports 16xE1 or 16xDS1 tributaries on compact HDR connectors.The DAC 16xV3 is compatible with and can be safely used in all cases with the DAC 16xV2,over the air, and in applications like NCM/SPDH/NTU, where a same DS1 can be insertedvia a DAC16Xv3 card(s) in one INU and then dropped on the facing side of the hop (or at anINU further down in the network) via DACxV2 card(s), and vice-versa.NOTE: An INU with a protected pair of DAC16xV3 cards can interface overthe air with an INU equipped with a protected pair DAC16xV2 to carry thesame DS1’s.48 JULY 2018 AVIAT NETWORKS
SYSTEM OVERVIEW CHAPTER 3Features additional to those provided by DAC 16x include:lTributary protectionlEthernet over E1/DS1 tribslIndividual line code selection for AMI or B8ZS on DS1 tribsFigure 12. DAC 16xV2DAC 4XDAC 4x supports 4xE1 or 4xDS1 tributaries on individual RJ-45 connectors. It also supportsE1 waysides on the STM1+1E1 link option.Figure 13. DAC 4XDAC 3xE3/DS3DAC 3xE3/DS3 supports 3xE3 or 3xDS3 tributaries on paired mini-BNC connectors.Figure 14. DAC 3xE3/DS3DAC 3xE3/DS3MDAC 3xE3/DS3M supports four operational modes:lNormal E3/DS3 tributary operation (as for DAC 3xE3/DS3)lE13 multiplexer mode. One or two E3 interfaces are multiplexed to an NxE1backplane.lM13 multiplexer mode. One or two DS3 interfaces are multiplexed to an NxDS1backplane.l34 Mbit/s transparent E3 mode for video (MPEG) transport. One or twotransparent E3 tributaries are each mapped to a 34xE1 backplane.lDS3 Ethernet mode to enable up to 43 Mbit/s Ethernet over legacy TDM radio orleased-line links (links must support transparent DS3).Tribs are supported on paired mini-BNC connectors.AVIAT NETWORKS JULY 2018 49
CHAPTER 3SYSTEM OVERVIEWFigure 15. DAC 3xE3/DS3MDAC 2x155eDAC 2x155e supports two STM1 electrical tributaries on paired BNC connectors.Figure 16. DAC 2x155eDAC 1x155oDAC 1x155o supports one STM1/OC3 single-mode optical tributary on SC connectors.Figure 17. DAC 1x155oDAC 2x155oDAC 2x155o supports two STM1/OC3 single-mode optical tributaries on SC connectors.Figure 18. DAC 2x155oDAC 155oMDAC 155oM multiplexes an STM1/OC3 optical tributary to an NxE1 or NxDS1 backplane. Theuser interface is provided on an SFP optical transceiver. Different SFPs support 1310nmsingle-mode, or 850nm multi-mode.It functions as a terminal multiplexer; it terminates or originates the STM1/OC3 frame. Itdoes not support interconnection of ADMs as there is no provision to transport STM1/OC3overheads for ADM to ADM synchronization.In virtual tributary mode it transports up to 130 Mbit/s Ethernet over an STM1/OC3 link.Options are provided for external/recovered, or internal clock sourcing.50 JULY 2018 AVIAT NETWORKS
SYSTEM OVERVIEW CHAPTER 3Figure 19. DAC 155oMDAC 155eMDAC 155eM multiplexes an STM1/OC3 electrical tributary to an NxE1 or NxDS1 backplane.The user interface is provided on an SFP electrical transceiver.It functions as a terminal multiplexer; it terminates or originates the STM1/OC3 frame. Itdoes not support interconnection of ADMs as there is no provision to transport STM1/OC3overheads for ADM to ADM synchronization.In virtual tributary mode it transports up to 130 Mbit/s Ethernet over an STM1/OC3 link.Options are provided for external/recovered, or internal clock sourcing.Figure 20. DAC 155oMNCMNCM provides an NxE1/DS1 loop switch capability. At ring nodes it is configured to accessredundant east and west traffic streams for data input (insert) and output (drop).lTraffic inserted into a local tributary is transmitted on both east and west facingstreams to create a bi-directional ring.lA local drop selection is made on these east and west streams on the receivedirection to use.lOperation applies on either framed or unframed E1/DS1 tributaries.lThe operational mode is low latency, non-hitless.Figure 21. NCMAUXAUX provides synchronous and/or asynchronous auxiliary data channels, NMS porting, andalarm input and output functions. Data options are sync at 64 kbps or async to 19.2 kbps.Figure 22.AVIAT NETWORKS JULY 2018 51
CHAPTER 3SYSTEM OVERVIEWNCCThe NCC is a mandatory plug-in for an INU/INUe. It performs key node management andcontrol functions, and provides various dc rails from the -48 Vdc input. It also incorporatesa plug-in flash card, which holds Node configuration and license data.Power input limits are -40.5 to -60 Vdc. The power connector is a D-Sub M/F 2W2. The+ve dc return pin is connected to chassis ground.Figure 23. NCCFANThe FAN is a mandatory plug-in. There are two variants, 2RU and 1RU. Each is fitted withtwo long-life axial fans plus monitoring and control circuits.One 1RU FAN is fitted in an INU.One 2RU FAN or two 1RU FANs are fitted in the INUe. The 2RU FAN is standard.Figure 24. FAN (1RU)NPCNPC provides redundancy for the NCC backplane bus management and power supplyfunctions.Figure 25. NPCPCCThe PCC provides a voltage conversion function for use at locations where the power supplyis +24 Vdc. It converts +24 (19 to 36) Vdc to -56 Vdc for connection to the INU -48Vdc input. -56 Vdc represents the typical float voltage for a battery-backed -48 Vdc supply.One PCC supports:52 JULY 2018 AVIAT NETWORKS
SYSTEM OVERVIEW CHAPTER 3lUp to a 200W in air-conditioned installations (ambient max 250C / 770F).lUp to a 150W in non-air-conditioned installations (ambient max 450C / 113oF).Figure 26. PCCProtection OptionsThe Nodes offer link, interface, network, and platform protection options:Link/Path ProtectionHot-standby, space diversity, frequency diversity, or dual protection options are available.All RACs and their companion ODU or IRU 600 are protectable.RAC 70/7X does not support frequency diversity protection.Rx path switching (voting) is hitless/errorless; Tx switching is not hitless.A remote Tx switch is forced in the event of a silent Tx failure.Interface ProtectionEthernet, E1/DS1, E3/DS3 and STM1/OC3 interfaces can be hot-standby protected usingpaired (stacked) DACs.The protectable DACs are DAC GE3, DAC 16x V2/V3, DAC E3/DS3, DAC 3xE3/DS3M, DAC155o, DAC 2x155o, DAC 2x155e, DAC 155oM, DAC 155eM.The NCM is also protectable using paired NCMs.TDM InterfacesFor TDM DACs and for NCM front panel tributaries two interface protection configurationsare supported, tributary protection and always-on:Tributary ProtectionlY-cables connect the paired DACs/NCMs to customer equipment. (Y-cableprotection is not supported for DAC 155eM).lIn the Rx direction (from the customer) both DACs/NCMs receive data, but onlythe online Rx DAC/NCM sends this data to the backplane bus.lIn the Tx direction, the online Tx DAC/NCM sends data to customer equipment, theother mutes its Tx line interface.lThe connected equipment is not involved in the protection process.AVIAT NETWORKS JULY 2018 53
CHAPTER 3SYSTEM OVERVIEWTributary Always-OnlSeparate cables connect each DAC/NCM to customer equipment.lIn the Rx direction (from the customer) both DACs/NCMs receive data, but onlythe online Rx DAC/NCM sends this data to the backplane bus.lIn the transmit direction both DACs/NCMs send data to customer equipment, andthe customer equipment switches between these two always-on tributaries.lProtection switching is not hitless. Typical restoration times are between 80 msand 120 ms.Network/Data ProtectionEthernet ring and ladder network protection is provided using RSTP or ERP options.Ethernet data redundancy is provided on link-aggregated links using L1 or L2 options.PDH ring network protection is provided using Eclipse E1/DS1 Loopswitch or Super PDH(SPDHTM) configurations.Ethernet Ring and Ladder NetworksEclipse DAC GE3 supports two ring protection mechanisms, Ethernet Ring Protection (ERP,ITU-T G.8032v2) and RSTP (IEEE 802.1w).ERP is a fast-acting automatic protection switching (APS) protocol for Ethernet ringtopologies. Features include:Ethernet Link Aggregation ProtectionTraffic redundancy is supported on co-channel Ethernet links using L1 or L2 linkaggregation options. If one link fails, its traffic is recovered on the remaining link or links.While the reduced bandwidth may result in some traffic loss for low-priority traffic,appropriate QoS settings can be used to ensure security for all higher priority traffic.Loop Switch Ring ProtectionLoop switch operation employs the NCM for ring capacities to 50xE1 or 63xDS1, with trafficswitching at the local node level.Operation is based on redundant east/west facing rings.lTraffic inserted into a local tributary is transmitted in east and west directions tocreate a bi-directional ring.lAt a drop site traffic is selected from either the east or west direction. If theselected direction fails, the opposite direction is automatically switched intoservice.lOne or more radio paths can be replaced by a fiber or coax span using the DAC54 JULY 2018 AVIAT NETWORKS
SYSTEM OVERVIEW CHAPTER 3155oM or DAC 3xE3/DS3M.lThe operational mode is low latency, non-hitless.Super PDH Ring ProtectionSuper PDHTM supports ring capacities to 64xE1 or 84xDS1, with traffic switching at the nodelevel using a ring wrapping technique.Operation is based on east/west facing rings, one nominated as clockwise, the other anti-clockwise.lUnder normal no-fault conditions, all traffic is passed on the clockwise primaryring.lWhen a fault occurs, the secondary, anti-clockwise ring, provides the protectioncapacity needed. Traffic is looped onto the secondary ring at one side of the breakpoint, and off at the other side, to bypass the break.lOne or more radio paths can be replaced by a fiber span using the DAC 155oM.lOperation is not hitless.Platform ProtectionPlatform management functions provided by the NCC are protected using the NPC option toprotect essential backplane bus and power supply functions.lBus protection protects all circuit/tributary traffic (alarm I/O is not protected).lPower supply protection protects against an NCC power supply failure. If the NCCconverter or one of its supply rails fails, the NPC will take over withoutinterruption - and vice versa.Eclipse Packet Node and Data Packet PlaneData Packet PlaneDPP operation is enabled via direct cable connection between the front panel packet dataport on a RAC 70, RAC 60/60E, RAC 6X/6XE, and a front-panel port on a DAC GE3/GE.Customer traffic connected to the DACs is bridged to the RACs, and then to the RFtransceiver; the split-mount ODU 300hp or ODU 600, or the all-indoor IRU 600.Where required, customer data can also be sourced via the circuit-switched backplane,meaning both the DPP and backplane can be used to source/send traffic. This has specialrelevance where native mixed-mode IP + TDM traffic is to be sent over a Packet Nodewireless link; GigE IP traffic via the DPP, and TDM traffic via the backplane.AVIAT NETWORKS JULY 2018 55
CHAPTER 3SYSTEM OVERVIEWAdvanced Adaptive Coding and Modulation (ACM)Advanced ACM options are provided using RAC 70, RAC 60/60E or RAC 6X/6XE plug-ins.lAdaptive modulation maximizes use of available channel bandwidth.lCoding is used to extend throughput granularity by providing maximum throughputor maximum system gain options on each adaptive modulation rate.lACM operation requires a 2.048 or 1.544 Mbps Bus Connection Size.RAC 70 Adaptive Modulation (AM)AM uses one of ten automatically and dynamically switched modulations - QPSK, 16 QAM,32 QAM, 64 QAM, 128 QAM, 256 QAM, 512 QAM, 1024 QAM, 2048 QAM or 4096 QAM. For agiven RF channel bandwidth a two-fold improvement in data throughput is provided for achange from QPSK to 16 QAM, a three-fold improvement to 64 QAM, and a four-foldimprovement to 256 QAM.The adaptive modulation engine ensures that the highest modulation and hence highestthroughput is always provided based on link quality.Modulation switching is hitless/errorless.Ethernet connections enjoy real synergy through the QoS awareness on the DAC GE3 GigEswitch, and the service provisioning provided by any MPLS or PBB-TE network overlay.lAll high priority traffic, such as voice and video, continues to get through whenpath conditions are poor and modulation/capacity is reduced.lWhen path conditions are normal (good) best-effort lower priority traffic, such asemail and file transfers, enjoy data bandwidths that can be up to four times theguaranteed (QPSK) bandwidth.While adaptive modulation can also be used on PDH links and combined PDH and Ethernetlinks, unlike Ethernet there is no QoS synergy on PDH connections.lE1/DS1 connections are dropped in user-specified order when link capacity isreduced, and restored when capacity is increased.CodingModulation code options provide two sets of modulation states, one for maximumthroughput, the other for maximum gain. These apply on each of the modulation rates(QPSK, 16 QAM, 64 QAM, 256 QAM) to provide a total of eight modulation states.Maximum throughput delivers maximum data throughput - at the expense of somesystem gain.Maximum gain delivers best system gain - at the expense of some throughput.56 JULY 2018 AVIAT NETWORKS
SYSTEM OVERVIEW CHAPTER 3Up to four of the eight modulation states offered with ACM can be selected for use. Forexample:lWith four modulation rates, each can be set for maximum throughput ormaximum gain.lWith three modulation rates, such as 16 QAM, 64 QAM, 256 QAM, one rate (any)can be set for maximum gain and additionally for maximum throughput, to providefour step AM operation.lWith two modulation rates, such as 16 QAM (or 64 QAM) with 256 QAM, each canbe set for maximum gain and additionally for maximum throughput, to providefour step AM operation.This feature provides a practical trade-off between capacity and system gain to fine-tunelink performance. It provides best balance on AM operation.lThe four modulation rates support near-linear 2x, 3x, 4x capacity steps.lThe coding options allow capacity/gain variations on these rates to always supportup to four steps, even when just two of the possible four modulation rates are inuse, or are permitted.lEven where just one modulation rate is required/permitted, the coding optionsupports two-step AM operation, one for maximum throughput, one for maximumgain.PlatformsEclipse supports flexible customization of traffic type, traffic capacity, and traffic protectionfor up to three links using the INU, and to six links using the INUe.For slot location and usage, cross-connects, capacity, and RAC/RFU parameters see:Platform Layout on page 57Slot Assignments on page 58Platforms on page 57Platform LayoutThe following table lists INU and INUe platform support for:lNon-protected and protected/diversity linkslSlot availability for option plug-inslOver-air data types supportedlODU and IRU 600 optionsAVIAT NETWORKS JULY 2018 57
CHAPTER 3SYSTEM OVERVIEWINU Supports 3 non-protected links or 1 protected/diversityand 1 non-protected link.INUe Supports up to 6 non-protected links for:1 protected/diversity and 4 non-protected links, or2 protected/diversity and 2 non-protected links, or3 protected/diversity links.IRU 600 IRU 600:QPSK to 256 QAM, 4 to 11 GHz ANSI licensed bands,5.8 GHz ISM band (USA and Canada).Requires RAC 60/RAC 6X or RAC 60E/6XE. Fixed oradaptive modulation rates.1+1 optimized.Extra-high Power, high-power, standard power RFUoptions.Three variants: V1, V2, V3. V1 and V2 are 3RU. V3 is2RU. V2 and V3 incorporate a Tx coaxial switch forHSB and MHSB/SD operation. (V1 is discontinued).Slot AssignmentsINU/INUe SlotsINU Slots 1, 2, 3, 4 are universal: any RAC, DAC, NCM, orAUX plug-inSlot 4 is NPC or universal: NPC or any RAC, DAC,NCM, AUXNCC and FAN slots are dedicatedFor protected operation the RAC/RAC, RAC/DAC155oM, NCM/NCM, or DAC/DAC pairings can beinstalled in any of the universal slots58 JULY 2018 AVIAT NETWORKS
SYSTEM OVERVIEW CHAPTER 3INU/INUe SlotsINUe Slots 1, 2, 3, 4, 5, 6 are universal: any RAC, DAC,NCM, or AUX plug-inSlots 7, 8, 9 are restricted: any DAC, NCM, or AUX,except DAC 155oM/eM and AUX where NMS access isrequired1Slot 10 is restricted: NPC option onlyNCC and FAN slots are dedicated - the INUe issupplied standard with a single 2RU FAN, thoughaccepts two 1RU FANsRAC/RAC, or RAC/DAC 155oM/eM protected pairingsmust be installed in the positions indicated by thearrowsFor protected DACs or NCMs, the protectionpartners can be installed in slots 1 to 9, except forthe DAC 155oM/eM where NMS access is needed, inwhich case install only in slots 1 to 61Internal (backplane bus) NMS access is only provided on slots 1 to 6. Do not install DAC155oM, DAC 155eM, or AUX in slots 7 to 9 if an NMS connection is required in theirconfiguration.AVIAT NETWORKS JULY 2018 59
CHAPTER 3SYSTEM OVERVIEWEclipse TerminalsEclipse Terminals (IDUs) are single-link radios. For network (multi-link) applications theyare back-to-back connected via their tributary ports at intermediate sites. Most can bepaired for protected link operation.IDUs may also be over-air interfaced to like IDUs of higher or lower ultimate capacity and,with the exception of the IDUsp, to Eclipse Node.All IDUs support split-mount installation; only IDU GE3 16x supports split-mount or all-indoor.NOTE: All IDUs with the exception of IDU GE3 16x and IDU 155o arelegacy IDUs (no longer manufactured).Refer to:300 Series Indoor Units on page 60Eclipse Radio Frequency Units on page 67Figure 27. Eclipse Terminal300 Series Indoor UnitsIDU 300 variants support Ethernet, PDH, SDH, on ETSI and ANSI bands.60 JULY 2018 AVIAT NETWORKS
SYSTEM OVERVIEW CHAPTER 3Table 4. Current IDU 300 VariantsApplication Variant Capacities ModulationE1/DS1 only IDU 30020xV25x, 10x, 20x, 32x, 40xE1, or4x, 8x, 16x, 28x, 32xDS1QPSK to 128QAMIDUsp 4x 4xE1 QPSKIDUsp 16x 4x, 8x, 16xE1 QPSKSTM1/OC3 IDU 155o STM1/OC3 16/64/128QAMEthernet withE1/DS1tributary optionsIDU ES Airlink capacities to 200 Mbps with up to 8xE1/DS1tribs.Ethernet interfaces: 4x 10/100Base-T.QPSK to 256QAMIDU GE 20x Airlink capacities to 360 Mbps and up to 20xE1/DS1tribs.Ethernet interfaces: 2x 10/100/1000Base-T plus2x SFP slots for 1000Base-LX optical 1310nm,1000Base-SX optical 850nm, or 1000Base-Telectrical.QPSK to 256QAMIDU GE3 16x Airlink capacities to 366 Mbps and to 16xE1/DS1 tribs.Ethernet interfaces: 4x 10/100/1000Base-T plus 2x SFPslots for optical or electrical transceiver options.QPSK to 256QAM withfixed or adaptivemodulationSplit-mount ODU options support operation on bands 5 to 38 GHz.All-indoor IRU 600 options support operation on ANSI bands L6 to 11 GHz, or 5.8 GHzunlicensed band (USA and Canada only), with IDU GE3 16x only.IDU 300 Series OverviewIDUs, except for IDUsp, can be over-air interfaced to an Eclipse Node. This applies only tonon-protected 1+0 link operation. Where 1+1 IDU operation is required, protected IDUsmust be installed at both link ends.IDU GE3 16xIDU GE3 16x is a state-of-art sub-compact radio terminal for all-IP and hybrid wirelessbackhaul. Its internal modules comprise relevant RAC 60E, DAC GE3, DAC 16xV2, AUX andNCC functions of Eclipse Node. Features include:lSplit-mount with ODU 300 or ODU 600 on licensed bands 5 to 38 GHzlAll-indoor with IRU 600 on ANSI licensed bands 4 to 11 GHzlAll-indoor with IRU 600 on license-free 5.8 GHz ISM band (USA, Canada, only)l256 QAM adaptive modulationlExtensive IP traffic management and monitoring capabilitieslPacket-synchronization optionslFlexible IP or hybrid IP+PDH link operationlBroad diagnostic functionslSub-compact, 1/2RU rack-printAVIAT NETWORKS JULY 2018 61
CHAPTER 3SYSTEM OVERVIEWlLow power consumption (less than 30W) for simplified power supply and coolingmanagementlAuxiliary data and alarm I/O optionslInter-operation with Eclipse Packet NodelOptional NEBS complianceRFU options are the ODU 300hp or ODU 300sp for split-mount operation, or the IRU 600 forall-indoor.Figure 28. IDU GE3 16xCapacity is licensed. Feature licenses apply to adaptive modulation, synchronous Ethernet,TDM tributary access, advanced QoS.Adaptive or Fixed ModulationFixed and adaptive modulation options are available.Adaptive modulation enables automatic adjustment of modulation and/or coding so that themost data efficient (highest possible) modulation is used over the prevailing path conditions.lAdaptive modulation refers to the dynamic adjustment of modulation rate.lCoding refers to an ability to set individual modulation rates for maximumthroughput, or maximum system gain.IDG GE3 supports four modulation rates, QPSK, 16 QAM, 64 QAM, or 256 QAM, plus acoding option on each for a total of eight modulation states. Plus any of the modulation statescan be separately selected for fixed operation.Hot Standby or Diversity ProtectionPaired IDUs support 1+1 hot standby or space diversity operation.Ethernet and E1/DS1 interface protection options are enabled with protected IDUs.Carrier Class Ethernet FeaturesThe Gigabit L2 switch capabilities include Synchronous Ethernet, 1+1 interface protection,and superior packet buffering and queuing.l6 user ports; 4x RJ-45; 2x SFP with optical or electrical transceiver optionsl8 priority queues per portl1+1 interface protection on protected IDUslPort and protocol-based priority assignment (MPLS Exp, DSCP, 802.1p)lTrTCM traffic policinglStrict, DWRR (Deficit Weighted Round Robin), and Hybrid scheduling modeslVLAN tagging, untagging, filtering, and translationlSynchronous Ethernet62 JULY 2018 AVIAT NETWORKS
SYSTEM OVERVIEW CHAPTER 3lLayer 2 link aggregation, IEEE 802.1AX static and dynamic (LACP)lRing/mesh Protection, ERP (ITU-T G.8032v2) and RSTP (IEEE 802.1w)lEthernet Service OAM (IEEE 802.1ag, and ITU-T under Y.1731)lStorm controllFlexible allocation of 1500 Kbytes of buffer memory.lJumbo frames to 10 Kbytes bi-directionallFlow controllIFG and Preamble suppressionAn IDU GE3 16x 1+0 terminal can be over-air interfaced to an Eclipse Packet Nodecomprising the INU, RAC 60/60E, DAC GE3 (or DAC GE, DAC ES) with ODU 600, ODU 300hpor IRU 600. Where E1 or DS1 side channels are required, a DAC 16xV2 should be installed inthe INU. Similarly an AUX is installed where external Alarm I/O interfaces are required.For protected IDU GE3 16x operation, both ends of the link must be IDU GE3 16x.IDU 155oIDU 155o supports a single 155 Mbps STM1/OC3 tributary on optical SC connectors.Modulations options are 16, 64 or 128 QAM.Figure 29. IDU 155oIDUs are paired to support 1+1 hot-standby or space diversity operation. Optical Y cablesare used to provide common Tx and Rx interfaces.Tx switching is not hitless.Rx switching (voting) is hitless (errorless).Synchronous or asynchronous auxiliary data and alarm I/O options are included.Requires ODU 300hp or ODU 300ep.IDU 155o can be over-air interfaced to an Eclipse Node comprising the INU, DAC 155o,2x155o, or 2x155e, and ODU 300. An AUX is installed where auxiliary channel services arealso required. This applies only to non-protected 1+0 link operation. Where 1+1 IDUoperation is required, protected IDUs must be installed at both link ends.IDU300 20xV2IDU 300 20xV2 supports 20 tributaries on individual RJ-45 connectors for E1 or DS1operation, modulation options to 128 QAM, and over-air capacities to 40xE1 or 32xDS1.Features include:Capacities to 20xE1 / 16xDS1 for single link non-protected operation.Capacities to 20xE1 or 16xDS1 for hot-standby or space diversity operation.AVIAT NETWORKS JULY 2018 63
CHAPTER 3SYSTEM OVERVIEWCapacities to 40xE1 or 32xDS1 for hot-standby operation.IDUs are paired for protected/diversity operation.For capacities to 20xE1 / 16xDS1 normal IDU equipment and path protection applies,with Y cables used on the tribs.For higher capacities, traffic from the standby IDU is routed to the online IDU to supporttermination of up to 40xE1 or 32xDS1 tribs. In this configuration tributary and PSUprotection is not supported, however RAC/ODU and path protection functions areretained.Tx switching is not hitless.Rx path switching (voting) is hitless (errorless) for capacities to 20xE1 /16xDS1. It is nothitless when configured for 40xE1 / 32xDS1 operation.Figure 30. IDU 300 20xV2IDU 300 20xV2 is capacity licensed. The base configuration supports 20xE1/16xDS1, withcapacities to 40xE1 or 32xDS1 obtained by requesting additional capacity upgrades at time oforder or as field-downloadable software licenses. See Licensing.Synchronous or asynchronous auxiliary data and alarm I/O options are included.Requires ODU 300hp, ODU 300ep, or ODU 300sp.IDU 300 20xV2 can be over-air interfaced to an Eclipse Node comprising the INU, DAC 16xand ODU 300. An AUX is installed where auxiliary channel services are also required. Thisapplies only to non-protected 1+0 (20xE1 / 16xDS1 max) link operation. Where 1+1 IDUoperation is required, protected IDUs must be installed at both link ends.IDUsp 16x and IDUsp 4xThese IDUs are cost optimized for basic E1 services:IDUsp 4x: 4xE1 with QPSK modulation.IDUsp 16x: 4x, 8x, 16xE1 with QPSK modulation.Figure 31. IDUsp 16xPaired IDUsp 16x IDUs support hot-standby operation; Tx and Rx switching is not hitless.The IDUsp 4x is not protectable.A single 64 kb synchronous auxiliary data connection is included; there is no alarm I/O.IDUsp requires an ODU 300sp or ODU 300hp; ODU 300ep is not supported.64 JULY 2018 AVIAT NETWORKS
SYSTEM OVERVIEW CHAPTER 3NMS connection is Ethernet-only; there is no serial interface for Portal PC connection.Instead the IDU is configured as a DHCP (Dynamic Host Configuration Protocol) server andthe Portal PC as a client.IDU ESIDU ES supports Fast Ethernet to 200 Mbps to provide an uncomplicated and cost effectivealternative to fiber. Its Layer 2 switch supports four customer 10/100base-T ports, twoover-air transport channels and comprehensive QoS options.Data throughput options range from 20 to 200 Mbps, and depending on the selectedthroughput, channel bandwidth ranges from 7 to 56 MHz, with modulation options fromQPSK to 256 QAM.Link capacity may be fully assigned to Ethernet traffic, or between Ethernet and up to 8wayside E1/DS1 circuits.Inter-frame gap (IFG) and preamble stripping and re-insertion is used across the link tomaximize Ethernet throughputs.Capacity is licensed. The base configuration supports a 20 Mbps data throughput, withhigher capacities to 200 Mbps obtained by requesting additional capacity upgrades at time oforder, or as field-downloadable software licenses.Protected 1+1 operation is not supported.Figure 32. IDU ESIDU ES is included in Aviat Networks’ Connect ES link package; a package comprising twoterminals, each with one IDU ES, and one ODU 300 outdoor unit, which depending on therequired throughput can be ODU 300sp, hp or ep.Synchronous or asynchronous auxiliary data and alarm I/O options are included.Requires ODU 300hp, ODU 300ep, or ODU 300sp.IDU ES can be over-air interfaced to an Eclipse Node comprising the INU, DAC ES and ODU300. Where E1/DS1 side channels are required a DAC 4x or DAC 16x is also installed.Similarly an AUX is installed where auxiliary channel services are required.IDU GE 20xIDU GE 20x supports Gigabit Ethernet plus up to 20xE1 or 20xDS1 waysides.Its Layer 2 switch supports two customer 10/100/1000base-T electrical ports, and anoptional SFP port for either 1000Base-X optical or 1000Base-T electrical. These interface toone or two transport (link) channels using transparent, VLAN or mixed operational modes.AVIAT NETWORKS JULY 2018 65
CHAPTER 3SYSTEM OVERVIEWSwitch features include RWPR (Resilient Wireless Packet Ring), layer 2 link aggregation,and comprehensive QoS options with VLAN tagging and jumbo frame support.Depending on the required Ethernet throughput, channel bandwidth ranges from 7 to 56 MHzETSI, and 5 to 80 MHz ANSI, with modulation options from QPSK to 256 QAM. MaximumEthernet throughput is 360 Mbps using one or both transport channels.Configured link capacity may be assigned to Ethernet, or between Ethernet and up to 20xE1or 20xDS1 side circuits, or to E1 or DS1 circuits only to a maximum of 20xE1 or 16xDS1.Inter-frame gap (IFG) and preamble stripping and re-insertion is used to maximize datathroughput.Capacity is licensed. The base configuration (no license required) supports 20xE1 or 20xDS1circuits. The licensed extensions enable Ethernet in steps to 50, 100, 150, 200, or 360 Mbps,each with up to 20xE1 or 20xDS1 waysides. See Licensing.Protected 1+1 hot-standby or space diversity operation is configured by adding a second IDUGE 20x. Ethernet traffic is supported on a single interface to one of the IDUs. E1/DS1 trafficis supported on interfaces to both IDUs using Y-cables.The 1RU IDU GE 20x complies with ETSI half-rack mechanical specifications with a rackdepth of 240 mm (9.4”).Figure 33. IDU GE 20xIDU GE 20x is also available in a ‘Connect’ link package, where a package comprises twoterminals, each with one IDU GE 20x, and one ODU 300 outdoor unit, which depending on therequired throughput and band, can be ODU 300sp, hp or ep.Alarm I/O options are included.An IDU GE 20x 1+0 terminal can be over-air interfaced to an Eclipse Node comprising theINU, RAC 30 or RAC 3X, DAC GE or DAC ES, and ODU 300. Where E1 or DS1 side channelsare required, a DAC 4x or DAC 16x is also installed. Similarly an AUX is installed whereexternal Alarm I/O interfaces are required.For protected IDU GE 20x operation, both ends of the link must be IDU GE 20x.66 JULY 2018 AVIAT NETWORKS
SYSTEM OVERVIEW CHAPTER 3Eclipse Radio Frequency UnitsODUs support split-mount installations. A rack-mounting IRU 600 is installed for all-indoorinstallation.IRU 600The IRU 600 is a rack-mounted transceiver unit for co-location with an INU/INUe as an all-indoor installation.lIRU 600 is 1+1 optimized. It comprises one or two RFUs (radio frequency units),and a filter-based ACU (antenna coupler unit).oThe ACU design supports paired and unpaired Tx/Rx frequency splits andincorporates an optional expansion port to allow other radio links onto itswaveguide feed for co-path operation.oProtected/diversity options include:n1+1 hot-standbyn1+0 hot-standby-readynSpace diversity (dual antennas) with common or split TxnFrequency diversity (single antenna) or frequency diversity with spacediversity (dual antennas)o1+0 repeater (back-to-back) single chassis operation is supported. The linksmay be in the same or different bands.o2+0 (or 2+2 using dual IRU 600 chassis) single antenna.lOperation encompasses ANSI 4/L6/U6/UU6, 7/8, 10, 11 GHz licensed bands, andthe FCC / Industry Canada 5.8 GHz unlicensed (ISM) band.oIRU 600v2 has been supplied for the 4/L6/U6, 7/8, 10 and 11 GHz licensedbands, and 5.8 GHz unlicensed band.oWith the introduction of IRU 600v3/v4:nIRU 600v3/v4 is supplied on bands 5.8, L6/U6/UU6, 11 GHz.nIRU 600v2 is supplied on all bands 7/8, 10 GHz.lFixed or adaptive modulation profiles are supported.lIRU 600 is only supported from a RAC 70, RAC 60/6X, or RAC 60E/6XE.lWhen multiple IRU 600 links are combined onto a single waveguide feed for ACCPoperation, required minimum Tx to Tx and Rx to Rx spacings, and minimum Tx toRx separations must be strictly maintained. For information on ACCP operationAVIAT NETWORKS JULY 2018 67
CHAPTER 3SYSTEM OVERVIEWand limitations contact Aviat Networks or your supplier.lEMI filtering is NEBS compliant.NOTE: Unless otherwise stated, reference to IRU 600 refers to all IRU600 variants.IRU 600 VariantsThere are four variants: IRU 600v4, IRU 600v3, IRU 600v2, IRU 600(v1). IRU 600(v1) isdiscontinued.IRU 600v4Figure 34. IRU 600v4 Front and Side ViewsIRU 600v4 is available with two RFU variants, one for Standard Tx power (SP) or High Txpower (HP), and one for Extra High Tx power (EHP).IRU 600v3/v4IRU 600v3/v4 is available with two RFU variants, one for standard Tx power (Std) or high Txpower (HP), and one for extra high Tx power (EHP).68 JULY 2018 AVIAT NETWORKS
SYSTEM OVERVIEW CHAPTER 3IRU 600v2 and IRU 600(v1)Both support two RFU variants, a standard Tx power (Std) RFU, and a high Tx power (HP)RFU.Tx Coaxial Switch: IRU 600v4, IRU 600v3 and IRU 600v2Primary benefits of the Tx coaxial switch are reduced power loss and faster Tx protectionswitch times.lIt avoids the losses associated with a Tx coupler/combiner.oWith the Tx coaxial switch (relay) there is no A-side versus B-sideconsideration required as the loss is not more than 0.5 dB on both. See ACULosses, IRU 600 on page 1.lFor details on average recovery times, see Appendix G.MHSB mode increases power consumption as both transmitters are fully active - bothonline and offline Tx status is captured in real time. Where lower power consumption is thepriority, an option is provided to mute the offline Tx. For power consumption data See INUPower Supply.lWith MHSB operation both A-side and B-side transmit are fully monitored in realtime.lWith a Tx mute configured on the offline Tx, its Tx status can be monitored though ahealth monitoring facility whereby the Tx is turned on, checked and turned offagain. The turn-on period is adjustable between 0 (no health monitoring) and 240 in1 hour increments.lThe Mute Tx Offline selection is made in the RAC 70, RAC 60/60E/6x/6XE plug-insscreen.RFUsRFUv4 (IRU 600v4)lThere are two RFU variants, standard/high Tx power (SP/HP), and extra high Txpower (EHP):oAn HP feature license is required to enable high Tx power on the SP/HP RFU.oNo feature license is required for the EHP RFU, the EHP capability is inclusive.lThe DC supply for the SP/HP RFU is provided via the INU cable.lThe EHP RFU is additionally powered via a front-panel D-Sub M/F 2W2 connectorfor wide-mouth +/- 21 to 60 VDC supply. Both +ve and -ve pins are isolated fromground.oThe power connector (D-Sub M/F 2W2) and cable is identical to that used forthe INU.oThe integral DC/DC converter provides polarity protection, under/over voltageAVIAT NETWORKS JULY 2018 69
CHAPTER 3SYSTEM OVERVIEWshutdown, over-current limit, and thermal shutdown.oFor operation from +24 VDC supplies, the associated INU/INUe can be fittedwith a PCC to convert +24 VDC to - 48 VDC. Otherwise a suitable externalconverter can be used - contact Aviat Networks for details.lProtected operation for MHSB and MHSB/SD configurations uses a Tx coaxialswitch and an Rx coupler. Switch connection is via a DIN5 connector.oThe DIN5 connector is located on the right side of the RFUs together with theSMA connector for RF cable connection to the ACU/Coax switch.lINU (RAC 70, RAC 60E/6XE) connection is via a front panel SMA connector. AnSMA-to-SMA cable is included with each RFU.lRSSI access is provided on the front panel as meter test-probe points. Metal doton right of RFU for ground.lThe RFU is 1RU, half-width.lA front panel tri-color status LED indicates:oRed flashing during boot-upoGreen for normal operationoRed when in an alarmed stateoOrange when in standby mode (standby Tx RFU in an MHSB or MHSB/SDpairing)lIncludes three software-controlled, individually alarmed, cooling fans.RFUv3 (IRU 600v3/v4)lThere are two RFU variants, standard/high Tx power (Std/HP), and extra high Txpower (EHP):oAn HP feature license is required to enable high Tx power on the Std/HP RFU.oNo feature license is required for the EHP RFU, the EHP capability is inclusive.lThe DC supply for the Std/HP RFU is provided via the INU cable.lThe EHP RFU is additionally powered via a front-panel D-Sub M/F 2W2 connectorfor wide-mouth +/- 21 to 60 Vdc supply. Both +ve and -ve pins are isolated fromground.oThe power connector (D-Sub M/F 2W2) and cable is identical to that used forthe INU.oThe integral DC/DC converter provides polarity protection, under/over voltageshutdown, over-current limit, and thermal shutdown.oFor operation from +24 Vdc supplies, the associated INU/INUe can be fittedwith a PCC to convert +24 Vdc to - 48 Vdc. Otherwise a suitable externalconverter can be used - contact Aviat Networks for details.lProtected operation for HSB and HSB/SD configurations employs a Tx coaxialswitch and an Rx coupler. Switch connection is via a DIN5 connector.70 JULY 2018 AVIAT NETWORKS
SYSTEM OVERVIEW CHAPTER 3oThe DIN5 connector is located on the right side of the RFUs together with theSMA connector for RF cable connection to the ACU/Coax switch.lINU (RAC 70, RAC 60E/6XE) connection is via a front panel SMA connector. AnSMA-to-SMA cable is included with each RFU.lRSSI access is provided on the front panel as meter test-probe points.lPower consumption is reduced when Tx power output is lowered. Applies to bothATPC and manual control of Tx power.lThe RFU is 1RU, half-width.lA front panel tri-color status LED indicates:oRed flashing during boot-upoGreen for normal operationoRed when in an alarmed stateoOrange when in standby mode (standby Tx RFU in a HSB or HSB/SD pairing)lIncludes four SW-controlled, individually alarmed, cooling fans.RFUv2 (IRU 600v2)lThe standard (Std) Tx power RFU is powered via its INU cable.lThe high Tx power (HP) RFU is additionally powered via a front-panel D-Sub M/F2W2 connector for wide-mouth +/- 21 to 60 Vdc supply. Both +ve and -ve pins areisolated from ground.oThe power connector (D-Sub M/F 2W2) and cable is identical to that used forthe INU.oThe integral DC/DC converter provides polarity protection, under/over voltageshutdown, over-current limit, and thermal shutdown.oFor operation from +24 Vdc supplies, the associated INU/INUe can be fittedwith a PCC to convert +24 Vdc to - 48 Vdc. Otherwise a suitable externalconverter can be used - contact Aviat Networks for details.lProtected operation for HSB and HSB/SD configurations employs a Tx coaxialswitch and an Rx coupler. Switch connection is via a DIN5 connector.oThe DIN5 connector is located on the right side of the RFUs together with theSMA connector for RF cable connection to the ACU/Coax switch.lINU (RAC 60E/6XE) connection is via a front panel SMA connector. An SMA-to-SMA cable is included with each RFU.lRSSI access is provided on the front panel as meter test-probe points.lThe RFU is 1.5 RU, half-width.lIncludes two cooling fans, individually alarmed.AVIAT NETWORKS JULY 2018 71
CHAPTER 3SYSTEM OVERVIEWIRU 600 CompatibilityIRU 600(v1) and IRU 600v2 share a common 3RU chassis. Dimensions and mounting pointsfor V1 and V2 RFUs and ACUs are identical.IRU 600v3/v4 is housed in a compact 2RU chassis. While the ACU is unique to the V3, the V3RFUs (Std/HP or EHP) can be used in V1 and V2 chassis using an adapter kit (Part No. 179-530112-001).The following use guidelines apply:lV1 and V2 RFUs are compatible sparing partners EXCEPT for HSB configurationswhere the ACU incorporates a coaxial relay Tx switch (IRU 600v2/v3 ACUs). RFUV1 cannot control the Tx coaxial switch. This means that:oV1, V2 RFUs are interchangeable for configurations not using a Tx switch eg.FD, 2+0, SD split Tx, 1+0. Applies to V1 and V2 ACUs.oIn protected HSB or HSB-ready systems with a V1 ACU (Tx combining), a V2RFU can spare for a V1.oOn V2 ACUs configured to use a Tx switch, the V1 RFU cannot spare for a V2RFU.oV2 HP RFUs require installation of a separate power supply connection (+/- 21to 60 Vdc) to its front panel 2W2 power connector. A power cable is suppliedwith the RFU.lV3 RFUs can be installed in an IRU 600(v1) or IRU 600v2 chassis using an adapterkit, which increases V3 RFU unit height to match the mounting points provided forV1 and V2 RFUs.oThe V3 RFU (with adapter kit installed) can be used in non-protected andprotected (HSB or HSB/SD) V1 and V2 chassis.nIf installed in a V1 chassis Tx combining applies for HSB and HSB/SDconfigurations.nIf installed in a V2 chassis (with Tx protection switch) Tx switching appliesfor HSB and HSB/SD configurations.nIf a V3 Std/HP RFU is installed, an HP license must also be installed toenable the high Tx power option on the RFU.nIf a V3 EHP RFU is installed, a separate power supply connection (+/- 21 to60 Vdc) to its front panel 2W2 power connector is required. A power cableis supplied with the RFU.oV1 or V2 RFUs cannot be installed in a V3 chassis.lV1 and V2 ACUs are interchangeable. The V3 ACU is not.oA V1 ACU can be installed in a V2 chassis, and vice-versa.oV1 and V2 ACUs cannot be installed in a V3 chassis. Similarly a V3 ACU cannotbe installed in a V1 or V2 chassis.72 JULY 2018 AVIAT NETWORKS
SYSTEM OVERVIEW CHAPTER 3lAll IRUs are over-air compatible. For example, a 1+0 IRU 600(v1) may be linkedto a 1+0 IRU 600v2 or IRU 600v3. Similarly, 1+1 HSB IRU 600(v1) may be linked toa 1+1 HSB IRU 600v2 or IRU 600v3. Hybrid configurations are also supported,such as FD linked to SD split Tx.IRU 600v1 and IRU 600v2 share a common 3 RU chassis. Dimensions and mounting pointsfor V1 and V2 RFUs and ACUs are identical.IRU 600v3 and IRU 600v4 are housed in a compact 2 RU chassis. While the ACU is unique toeach of the V3 and V4, the V3 and V4 RFUs (SP/HP or EHP) can be used in V1 and V2 chassiswith existing v1 or v2 ACU using an adapter kit (Part N° 179- 530112-002) for V3 and (Part179-530508-001) for V4.The following use guidelines apply:lV1 and V2 RFUs are compatible sparing partners EXCEPT for HSB configurationswhere the ACU incorporates a coaxial relay Tx switch (IRU 600v2 ACUs). RFU V1cannot control the Tx coaxial switch. This means that:oV1, V2 RFUs are interchangeable for configurations not using a Tx switch eg.FD, 2+0, SD split Tx, 1+0. Applies to V1 and V2 ACUs.oIn protected HSB or HSB-ready systems with a V1 ACU (Tx using mute/unmuteinstead of using an RF Tx switch), a V2 RFU can spare for a V1 by alternativelyusing mute/unmute instead of attempting to control an RF Tx switch like a v2RFU normally does.oOn V2 ACUs configured to use a Tx switch, the V1 RFU cannot spare for a V2RFU.oV2 HP RFUs require installation of a separate power supply connection (+/- 21to 60 Vdc) to its front panel 2W2 power connector. A power cable is suppliedwith the RFU.lV3 and V4 RFUs can be installed in an IRU 600v1 or IRU 600v2 chassis using anadapter kit, which increases the V3 or V4 RFU unit height to match the mountingpoints provided for V1 and V2 RFUs.oThe V3 or V4 RFU (with adapter kit installed) can be used in non-protected andprotected (HSB or HSB/SD) V1 and V2 chassis.lIf installed in a 3 RMS chassis equipped with a V1 RFU, Tx combining applies forMHSB and MHSB/SD configurations.lIf installed in a 3 RMS chassis equipped with a V2 RFU, (with Tx protection switch)Tx switching applies for MHSB and MHSB/SD configurations.lIf a V3 or V4 SP/HP RFU is installed, an HP license must also be installed toenable the high Tx power option on the RFU.lIf a V3 or V4 EHP RFU is installed, a separate power supply connection (+/- 21 to60 VDC) to its front panel 2W2 power connector is required. A power cable issupplied with the RFU.lV1 or V2 RFUs cannot be installed in a V3 chassis.AVIAT NETWORKS JULY 2018 73
CHAPTER 3SYSTEM OVERVIEWlV1 and V2 ACUs are interchangeable. The V3 or V4 ACU is not.oA V1 ACU can be installed in a V2 chassis, and vice-versa.oV1 and V2 ACUs cannot be installed in a V3 or V4 chassis. Similarly, a V3 or V4ACU cannot be installed in a V1 or V2 chassis.lAll IRUs are over-air compatible when used with a same RAC on both sides of thehop. For example, a 1+0 IRU 600v1 may be linked to a 1+0 IRU 600v2 or IRU600v3, or IRU 600v4. Similarly, 1+1 HSB IRU 600v1 may be linked to a 1+1 HSBIRU 600v2 or IRU 600v3, or IRU 600v4. Hybrid configurations are also supported,such as FD linked to SD5.8 GHz Unlicensed BandThe RFU for the 5.8 GHz unlicensed band is common to the L6 licensed band for easytransition and sparing (from unlicensed to licensed and vice-versa). Links can be rapidlydeployed using 5.8 GHz unlicensed, and subsequently transitioned to L6 on license approval.lThe RFU is a high-power (HP) variantoWith IRU 600v2 the HP RFU is used.oWith IRU 600v3 the Std/HP RFU is used (the V3 EHP RFU is not presentlyavailable for use on the 5.8 GHz unlicensed band).nTo operate the V3 Std/HP RFU at high Tx power, an HP license must beinstalled.lThe 5.8 GHz unlicensed band is designed to support easy and fast deployment.With a suitable antenna, installation can be 'immediate'.lThe common 5.8 GHz / L6 RFU design means subsequent conversion to L6licensed operation only requires replacement of the ACU.NOTE: 5.8 GHz operation supports fast turn-up for new linkrequirements. On receipt of a license, operation can be converted to L6licensed band by replacing the ACU.Eclipse IDUs and INUs with IRU 600 are compliant with the relevant parts of FCC CFR47,Part 15.407, and Industry Canada RSS-210 Annex 8, on ISM frequency band 5725 to 5850MHz. International use is not supported; the system does not employ DFS and as suchcannot be deployed within Europe or any country where DFS is a regulatory requirement forprotection of radars.Features and Capabilities:lACU filters are tuned 30 MHz wide.oFilters are spot tuned (pre-tuned) on 5740.5/5805.5 MHz or 5769.5/5834.5MHz.oWith 30 MHz filters just two Tx/Rx pairs can be used to provide full coverage ofthe band.74 JULY 2018 AVIAT NETWORKS
SYSTEM OVERVIEW CHAPTER 3oOperation is designed to meet all regulatory requirements associated with 47CFR Part 15.407. As such, deployment is precluded within 0.5 Mhz of the bandedges to comply with band edge emission requirements.lBandwidths 5, 10, 20, or 30 MHz.lTx and Rx can be paired on different sub-bands (Tx on one 30 MHz sub-band, RX onthe other).lModulation can be adaptive (QPSK to 256 QAM), or fixed.lSupports Ethernet and/or NxDS1, NxDS3, or OC3 payloads, with air-linkcapacities to 189 Mbit/s (30 MHz Ch BW).lThe common 5.8 GHz and L6 RFU supports easy migration from one band to theother (from unlicensed to licensed and vice-versa).oRFUs can be retained during migration, but ACU must be replaced (not re-tuned).lExtensive protection and diversity options.lOutput power (at 5.8 GHz) is limited to 29 dBm at the antenna port to ensurecompliance with the FCC 1 Watt rule.lFor Tx power, power control, and system gain figures, see the Eclipse PacketNode ANSI Datasheet.Operational Limitations and RestrictionsUnlicensed band operation means sharing the air-space with other operators of unlicensedband links. interference is possible.lIRU 600 5.8 GHz operation is narrow-band (max 30 MHz) high-power; itcompetes/shares spectrum with other narrow-band links and with spread-spectrum links.lPerformance could deteriorate over time with the introduction of other links in thesame geographical area.lAntennas must be approved (FCC or Industry Canada) for the 5.8 GHz unlicensedband.oEclipse 5.8 GHz is certified for use with a parabolic antenna with a maximumgain of 45.9 dBi or a flat panel antenna with a maximum gain of 28 dBi.AVIAT NETWORKS JULY 2018 75
CHAPTER 3SYSTEM OVERVIEWEclipse LicensingEclipse Node, IDU GE3 16x, IDU GE 20x, IDU ES, and IDU 300 20xV2 are subject to capacitylicensing. Eclipse Node and IDU GE3 16x are additionally subject to feature licensing onadvanced features.Feature license operation is software release dependent. Ensure you have the relevantsoftware release installed. Refer to Licensing Requirements and Options on page 1.INUs:lFlexible Node-based Licensing applies for Eclipse Node and Packet Node toreplace/complement RAC-based licensing.lNode-based licensing requires SW release 5.0 or later. (SW 5.0 or later must beinstalled in a Node before installing or upgrading to Node-based licensing).lNode-based licensing is required for DPP operation and for feature licensing.lFeature Licensing applies on selected Node features. The licensed features are:oEZF-01: Layer 1 Link Aggregation (DAC GE). Traffic is between the links on abyte-by-byte basis, based on the capacity of the links. Unlike L2, it is fullyeffective for just one active session, such as between routers, or where thereare only a few concurrent sessions.oEZF-02: Adaptive Modulation (RAC 70, RAC 60/60E, RAC 6X/6XE). Packet Nodeadaptive coding and modulation (ACM) dynamically switches betweenmodulation selections.QPSK, 16 QAM, 64 QAM, 256 QAM, 512 QAM, or 1024QAM (2048 QAM, and 4096 QAM also on the RAC 70/7X). For the RAC60/6X/60E/6XE, code settings additionally provide two sets of rates for eachmodulation; one for maximum-throughput, the other for maximum-gain, toprovide eight modulation states in total.oEZF-03: Secure Management (NMS). Applies to Eclipse NMS access over thenetwork, and to local access via the Portal craft tool. It also enables securemanagement access to Eclipse over an unsecured network, and protectsEclipse configurations from accidental or intentional modification byunauthorized personnel.oEZF-04: Payload Encryption (RAC 70, RAC 60/60E, 6X/6XE). Encrypts all trafficand management data over the wireless link to prevent eavesdropping.oEZF-05: Ethernet over TDM (DS3, E1, DS1). Enables mapping of Ethernet datato DS3, E1, or DS1 PDH interfaces using the DAC 3xDS3M or DAC 16x V2/V3.Supports transport of Ethernet data over existing DS3 or NxE1/DS1 radio orleased-line circuits.oEZF-06: RADIUS Client. Enables connection validation to a radius server for76 JULY 2018 AVIAT NETWORKS
SYSTEM OVERVIEW CHAPTER 3centralized account management.oEZF-09: Synchronous Ethernet. Enables Synchronous Ethernet operation onthe DAC GE3.oEZF-10: Ethernet OAM. Enables access to Ethernet Service OAM capabilities.oEZF-14 and EZF-1408: TDM Loop SwitchnEZF-1408 supports up to 8xE1/DS1 circuits (the max number ofdrop/insert tributaries supported on the NCM front panel).nEZF-14 supports up to 50xE1 or 63xDS1 tributary circuits (the max numberof drop/insert tributaries supported on an INU/INUe - requires NCMtogether with DXR 16xV2 plug-ins).oEZF-42: FIPS 140-2 Secure Operation. Enables secure management of Eclipsein compliance with the Federal Information Processing Standard (FIPS)Publication 140-2. Applies to the INUe only.oEZF-48: FIPS 140-2 + UC-APL Secure Operation. Enables secure managementof Eclipse in compliance with the Federal Information Processing Standard(FIPS) Publication 140-2, also includes Unified Capabilities (UC) ApprovedProducts List (APL) compliance. Applies to the INUe only.oEZF-43: Enables IPv6 operation. Includes OSPF IPv6 and RIPNG. Automaticallyenabled in software 8.1 or later.NOTE: When ODU 300 EP is present in the terminal, IPv4 address isrequired for software loading.oEZF-51 to EZF-56: ODU 600 high Tx power. Unlocks an additional 3dB oftransmit power over standard power. Applies to ODU 600 only, on allmodulations, on all bands. It also increases the manual and ATPC transmitpower control range by 3dB.nEZF-51: ODU 600 High power option 1 x ODUnEZF-52: ODU 600 Nodal High power option 2 x ODUnEZF-53: ODU 600 Nodal High power option 3 x ODUnEZF-54: ODU 600 Nodal High power option 4 x ODUnEZF-55: ODU 600 Nodal High power option 5 x ODUnEZF-56: ODU 600 Nodal High power option 6 x ODUoEZF-61 to EZF-66: IRU 600v3/v4 high Tx power. Unlocks an additional 3dB oftransmit power over standard power. Applies on all modulations, on all IRU600v3/v4 bands. It also increases the manual and ATPC transmit powercontrol range by 3dB.nEZF-61 EZG-61 IRU 600 High power option 1 x RFUnEZF-62 EZG-62 IRU 600 Nodal High power option 2 x RFUnEZF-63 EZG-63 IRU 600 Nodal High power option 3 x RFUnEZF-64 EZG-64 IRU 600 Nodal High power option 4 x RFUAVIAT NETWORKS JULY 2018 77
CHAPTER 3SYSTEM OVERVIEWnEZF-65 EZG-65 IRU 600 Nodal High power option 5 x RFUnEZF-66 EZG-66 IRU 600 Nodal High power option 6 x RFUlIDU licensing for all IDUs except IDU GE3 16x is unchanged.NOTE: You can upgrade to SW release 5.0 or higher and still continue touse RAC-based licensing but you will not have access to the benefitsprovided under Node-based licensing (DPP operation and licensedfeatures).All new Nodes ordered are default installed with the most recent SWrelease version. From SW release 5.0, can elect to use (order) a Node-based or RAC-based license.IDU GE3 16x:Capacity-based licensing and feature licensing applies on selected features.Capacity Licenses:lEZE-10020: 20 Mbit/slEZE-10050: 50 Mbit/slEZE-10100: 100 Mbit/slEZE-10150: 150 Mbit/slEZE-10200: 200 Mbit/slEZE-10400: 400 Mbit/sFeature Licenses:lEZF-10002: Adaptive ModulationlEZF-10003: Secure ManagementlEZF-10006: RADIUSlEZF-10009: Synchronous EthernetlEZF-10010: Ethernet OAMlEZF-10019: Enable TDM PortslEZF-10020: Advanced QoSlEZF-10043: Enables IPv6 operation. Includes OSPF IPv6 and RIPNG.Automatically enabled in software 8.1 or later.NOTE: When ODU 300 EP is present in the terminal, IPv4 address isrequired for software loading.lEZF-10051: ODU 600 high Tx power option 1 x ODU. Unlocks an additional 3dB oftransmit power over standard power. Applies to ODU 600 only, on allmodulations, on all bands. It also increases the manual and ATPC transmit powercontrol range by 3dB.lEZF-10061: IRU 600v3/v4 high Tx power option 1 x RFU. Unlocks an additional 3dBof transmit power over standard power. Applies on all modulations, on all IRU78 JULY 2018 AVIAT NETWORKS
SYSTEM OVERVIEW CHAPTER 3600v3/v4 bands. It also increases the manual and ATPC transmit power controlrange by 3dB.AVIAT NETWORKS JULY 2018 79
CHAPTER 3SYSTEM OVERVIEWEclipse Configuration and ManagementEclipse is a software-driven product; there are no manual controls. Configuration andmanagement is achieved via Portal and ProVision.Portal is a PC based configuration and diagnostics tool for Eclipse.ProVision is the Eclipse network element manager. ProVision also supports other AviatNetworks products, including legacy products.Portal is supported in the Eclipse system software, such that once installed on a PC, itautomatically downloads support from the radio as needed to ensure Portal alwaysmatches the version of system software supplied, or subsequently downloaded in any radioupgrade.Portal has the look and feel of a Windows environment with screen-based views andprompts for all configuration and diagnostic attributes.A Portal PC connects to an INU/INUe/IDU using Ethernet or V.24 options.For more information see Introduction to Portal.ProVision is the network element manager for all Aviat Networks radios (current andlegacy). ProVision also supports partner products, including multiplexors, switches,routers, and power systems.ProVision is installed on a Windows or Solaris server, typically at a network operatingcenter, and communicates with network elements using standard LAN/WAN IP addressingand routing; each radio has its own unique IP address.For more information about ProVision, refer to the Aviat Networks ProVision User Guide.Secure Access from Portal and ProVision is enabled through the Secure Management andRADIUS Client strong security options.80 JULY 2018 AVIAT NETWORKS
SYSTEM OVERVIEW CHAPTER 3Eclipse AntennasAntennas for operation on the 5.8GHz unlicensed band are (must be) FCC approved.lParabolic antennas for the 5.8 GHz unlicensed band must not exceed a maximumgain of 45.9 dBi.lFlat panel antennas for the 5.8 GHz unlicensed band must not exceed a maximumgain of 28 dBi.Antenna mounts are designed for use on industry-standard 115 mm OD (4.5 inch) pipe-mounts.AVIAT NETWORKS JULY 2018 81
CHAPTER 3SYSTEM OVERVIEWEclipse Power SupplyEclipse is designed to operate from a -48Vdc power supply (+ve earth) but will operate tospecification over a voltage range of -40.5 to -60Vdc.A plug-in PCC option for the INU provides a voltage conversion function for locations wherethe power supply is +24 Vdc. It converts +24 (19 to 36) Vdc to -56 Vdc for connection to theINU -48Vdc input. -56 Vdc represents the typical float voltage for a battery-backed -48 Vdcsupply.The PCC supports:lUp to a 200W in air-conditioned installations (ambient max 250C / 770F).lUp to a 150W in non-air-conditioned installations (ambient max 450C / 113oF).NOTE: An external +24 Vdc to -48 Vdc converter can be used instead ofthe PCC. Contact Aviat Networks for details.The dc power supply must be UL or IEC compliant for SELV (Safety Extra Low Voltage)output (60Vdc maximum limited).82 JULY 2018 AVIAT NETWORKS
INTRODUCTION TO ECLIPSE INSTALLATION CHAPTER 4Chapter 4. Introduction to Eclipse InstallationThis section covers installation procedures for Eclipse devices, from unpacking andchecking the equipment to completion of the physical installation and antenna alignment.This section includes:lInstallation Overview on page 84lBefore Going On Site on page 85For information on installing the Portal software to configure Eclipse, see Installing andConnecting Portal on page 1.NOTE: Eclipse has been tested for and meets EMC Directive 89/336/EEC.The equipment was tested using screened cable; if any other type ofcable is used, it may violate compliance.CAUTION: Eclipse is a Class A product. In a domestic environment it may cause radiointerference: be prepared to resolve this. Eclipse equipment is intended to be usedexclusively in telecommunications centers.WARNING: You must comply with the relevant health and safety practices whenworking on or around Eclipse radio equipment. Refer to the section on Health andSafety on page 25.AVIAT NETWORKS JULY 2018 83
CHAPTER 4INTRODUCTION TO ECLIPSE INSTALLATIONInstallation OverviewThis section provides a basic guide, in order, of an Eclipse hardware installation process.Installation can be completed up to antenna alignment without the use of Eclipse Portal, thePC based craft tool. Portal is required to check and configure an Eclipse Node or Terminal.Hardware installation typically proceeds as follows:1. Pre-InstallationlUnpack equipment - see Unpacking the Eclipse Equipment on page 86lVerify system configuration:lCheck basic componentslCheck kits and accessories2. InstallationlAntenna - see See "Installing the Antenna"lODU - see ODU Installation on page 1lIRU 600 - see IRU 600 Installation on page 87lINU / IDU chassis - see Installing the INU and INUe on page 101 or See "Installingthe IDU".lINU plug-in cards - see Plug-in Installation Requirements on page 121lTraffic and NMS cables - as required84 JULY 2018 AVIAT NETWORKS
INTRODUCTION TO ECLIPSE INSTALLATION CHAPTER 4Before Going On SiteThis section includes:lInstallation Tools and Materials on page 85lUnpacking the Eclipse Equipment on page 86Installation Tools and MaterialsEnsure you have the following tools and material before going to site. These are items to besourced/supplied by the installer.The items are indicative for standard installations. For non-standard installations additionalmaterials and tools may be required.Table 5. Required Tools and MaterialEquipment Tool/Material DescriptionAntenna As required by themanufacturerRefer to the manufacturer’s data supplied with each antennafor required and recommended installation tools andequipment. (Aviat Networks offers antennas from severalsuppliers).Eclipse Radios Basic electrician’s toolkit The kit must include a crimp lugs, a crimp tool for attachingthe lugs to stranded copper cable, a multimeter, and for ODUpolarization rotator bolts, a set of metric Allen keys.Open-ended spanners 19mm (3/4 inch) open-ended spanner for attaching the ODUto the mounting collar.Torque wrench Capable of 66 N-m or 50 ft-lb, with a selection of sockets forantenna mount fasteningCrimp tool(s) for ODUcable connectorsThe correct crimp and cut-off tools must be used to avoiddamage to the cable outer and to ensure correct crimping ofthe connectors.Hot-air gun For use on the heat-shrink tubing that may be supplied withsome brands of TypeN connector.Protective grease andzinc-rich paintFor weather-protecting grounding attachment points ontowers and grounding bars.BNC cable To access the RSSI voltage at the ODU for antenna alignment.This could be a BNC to banana-plugs cable for connection to amultimeter. Such a cable is available as an optional accessoryRefer to Accessories in the Eclipse Product Ordering Guide.4mm2(#12) green PVCinsulated strand copperwire and grounding lugsFor grounding the indoor unit to the rack/frame16 mm2(#6) green PVCinsulated strand copperwire and grounding lugsFor grounding the rack to the station ground.16mm is also required for chassis grounding for NEBScompliance.AVIAT NETWORKS JULY 2018 85
CHAPTER 4INTRODUCTION TO ECLIPSE INSTALLATIONUnpacking the Eclipse EquipmentTo unpack Eclipse equipment:1. Open the shipping boxes, carefully remove the equipment and place it on a clean, flatworking surface.2. Ensure all the basic components and accessories for your system have been includedin the shipment by comparing the packaging, component part numbers and productdescriptions against the packing list, and cross-checking against the installationdatapack for the system to be installed.3. If there has been shipping damage or there are discrepancies between the equipmentexpected and the equipment received, contact an Aviat Networks Help Desk or yoursupplier.86 JULY 2018 AVIAT NETWORKS
IRU 600 INSTALLATION CHAPTER 5Chapter 5. IRU 600 InstallationNOTE: Before commissioning an IRU 600 and companion INU, itsantenna, waveguide, and waveguide pressurization equipment mustbe installed according to manufacturer’s instructions.For an overview of IRU 600 features and function, see IRU 600 on page 67.For information on installing an INU, see Installing the INU and INUe on page 101.For guidance on installing antennas, waveguide, and pressurization equipment, see the BestPractices Guide from Aviat Networks.IRU 600 (v1), IRU 600v2, and IRU 600v3/v4 RFU Sparing CompatibilityFor information on sparing compatibility see IRU 600 Compatibility on page 72.AVIAT NETWORKS JULY 2018 87
CHAPTER 5IRU 600 INSTALLATIONIRU 600 CompatibilityIRU 600v1 and IRU 600v2 share a common 3 RU chassis. Dimensions and mounting pointsfor V1 and V2 RFUs and ACUs are identical.IRU 600v3 and IRU 600v4 are housed in a compact 2 RU chassis. While the ACU is unique toeach of the V3 and V4, the V3 and V4 RFUs (SP/HP or EHP) can be used in V1 and V2 chassiswith existing v1 or v2 ACU using an adapter kit (Part N° 179-530112-002) for V3 and (Part N°179-530508-001) for V4.The following use guidelines apply:lV1 and V2 RFUs are compatible sparing partners EXCEPT for HSB configurationswhere the ACU incorporates a coaxial relay Tx switch (IRU 600v2 ACUs). RFU V1cannot control the Tx coaxial switch. This means that:oV1, V2 RFUs are interchangeable for configurations not using a Tx switch e.g.FD, 2+0, SD split Tx, 1+0. Applies to V1 and V2 ACUs.oIn protected HSB or HSB-ready systems with a V1 ACU (Tx using mute/unmuteinstead of using an RF Tx switch), a V2 RFU can spare for a V1 by alternativelyusing mute/unmute instead of attempting to control an RF Tx switch like a v2RFU normally does.oOn V2 ACUs configured to use a Tx switch, the V1 RFU cannot spare for a V2RFU.oV2 HP RFUs require installation of a separate power supply connection (+/- 21to 60 Vdc) to its front panel 2W2 power connector. A power cable is suppliedwith the RFU.lV3 and V4 RFUs can be installed in an IRU 600v1 or IRU 600v2 chassis using anadapter kit, which increases the V3 or V4 RFU unit height to match the mountingpoints provided for V1 and V2 RFUs.oThe V3 or V4 RFU (with adapter kit installed) can be used in non-protected andprotected (HSB or HSB/SD) V1 and V2 chassis.lIf installed in a 3 RMS chassis equipped with a V1 RFU, Tx combining applies forMHSB and MHSB/SD configurations.lIf installed in a 3 RMS chassis equipped with a V2 RFU, (with Tx protection switch)lTx switching applies for MHSB and MHSB/SD configurations.lIf a V3 or V4 SP/HP RFU is installed, an HP license must also be installed toenable the high Tx power option on the RFU.lIf a V3 or V4 EHP RFU is installed, a separate power supply connection (+/- 21 to60 VDC) to its front panel 2W2 power connector is required. A power cable issupplied with the RFU.88 JULY 2018 AVIAT NETWORKS
IRU 600 INSTALLATION CHAPTER 5lV1 or V2 RFUs cannot be installed in a V3 chassis.lV1 and V2 ACUs are interchangeable. The V3 or V4 ACU is not.oA V1 ACU can be installed in a V2 chassis, and vice-versa.oV1 and V2 ACUs cannot be installed in a V3 or V4 chassis. Similarly, a V3 or V4ACU cannot be installed in a V1 or V2 chassis.lAll IRUs are over-air compatible when used with a same RAC on both sides of thehop.oFor example, a 1+0 IRU 600v1 may be linked to a 1+0 IRU 600v2 or IRU 600v3,or IRU 600v4. Similarly, 1+1 HSB IRU 600v1 may be linked to a 1+1 HSB IRU600v2 or IRU 600v3, or IRU 600v4. Hybrid configurations are also supported,such as FD linked to SD.Table 6. RAC Compatibility Over-Air Links Guidelines and Examples:IRU 600 RAC Link Direction IRU 600 RACV3 or V4 60/6X Same V4 or V3 60/6XV4 or V3 70/7X Same V3 or V4 70/7XV3 or V4 60/6X Independent V4 or V3 70/7XV4 or V3 70/7X Independent V3 or V4 60/6XAVIAT NETWORKS JULY 2018 89
CHAPTER 5IRU 600 INSTALLATIONIRU 600 Installation ProcedureThis procedure applies to IRU 600v4, IRU 600v3, IRU 600v2, and IRU 600(v1).lUnless otherwise stated, reference to IRU 600 refers to all IRU 600 variants.lUnless otherwise stated, reference to a V2 RFU refers to standard power (Std)and high-power (HP) variants.lUnless otherwise stated, reference to a V3/V4 RFU refers to standard power(Std), high-power (HP), and extra high-power (EHP) variants.The IRU 600v3/v4 Std/HP RFU is SW configured for standard or high-power. The HP optionrequires installation of HP feature license EZF-61 to 66, or EZG-61 to 66. See Node FeatureLicensing on page 1.See:lChassis Installation on page 90lChassis Grounding on page 93lWaveguide Installation on page 94lWaveguide Connection to ACU on page 94lPower Supply Connection on page 95lInsertion Loss Labels on page 97lIRU 600 Installation on page 87lExpansion Port Use on page 97lFAN Module on page 97lIRU 600 Installation on page 87lChassis Adapter Kit for IRU 600v3 and IRU 600v4 RFUs on page 98ChassisAdapter Kit for IRU 600v3 and IRU 600v4 RFUs on page 98Chassis Adapter Kit forIRU 600v3 and IRU 600v4 RFUs on page 98Chassis Installation1. Fit the rack mounting brackets onto the chassis.oBrackets can be mounted in either a forward mount or a flush mount position.oBrackets can be mounted such that the grounding stud is to the left or rightside.2. Install the chassis. If installing multiple chassis:oFor IRU 600(v1) and IRU 600v2 install with a 3RU space between the chassis topermit installation of an expansion or extension kit. This space can be used to90 JULY 2018 AVIAT NETWORKS
IRU 600 INSTALLATION CHAPTER 5install an INU/INUE/IDU GE3 16x.oFor IRU 600v3/v4 no chassis spacing is required, but a 1RU space should beretained above the top and below the bottom of the chassis stack to ease handaccess to RFU - ACU cable installation.3. Locate and secure RFU(s) and ACU in the IRU 600 chassis.oFor IRU 600v3/v4 the chassis-mounted post fitted to secure the right side ofthe RFU / left side of the ACU front cover is removable.oThis is to assist connection/dis-connection of the RFU SMA connectors, andthe DIN5 connector on 1+1 configurations.CAUTION: When re-fitting the IRU 600v3/v4 removable post do not over-tighten. Thumb-tighten only to avoid thread-striping.Figure 35. IRU 600v3 Removable Post4. Connect the RFU(s) to the ACU using the supplied RF cables. Refer to the cablingdiagram on the rear side of the ACU front panel. The lower RFU is A-side, the top B-side.A-side is the default online RFU in a 1+1 protected pairing.Figure 36. Example Cabling Diagram on Rear of ACU Front PanellFor IRU 600v2 and IRU 600v3/v4 ACUs fitted with a Tx coaxial switch, fit theRFU-to-switch cable assembly.oFor IRU 600v3/v4 the fixing post in front of the RFU connectors can be removedto aid connector access. See step 3 above.oEnsure cables connect to the correct RFU. Refer to the cabling diagram on therear side of the ACU front cover.oEnsure DIN5 RFU cable connectors are correctly inserted and locked usingthe connector locking ring - turn the ring clockwise until clicked into its lockedposition.oEnsure the switch connector is held secure using its screw fasteners.AVIAT NETWORKS JULY 2018 91
CHAPTER 5IRU 600 INSTALLATIONoThe Tx switch cable must remain securely connected at all times. Incorrectcommunication between the RFU and Tx switch may result in mismatched A-side and B-side operation and loss of standby.CAUTION: Check installation of DIN5 RFU cable connectors. The lock ring should homewith an audible click.NOTE: Multiple voltage pules are used to energize the Tx switch relay.lConnect the RFU(s) to the INU/INUe RAC 70, RAC 60/60E or RAC 6X/6XE card(s)using the supplied IF cable(s). The minimum bend radius of the IF cable is 25mm.lFor the IRU 600v2 HP RFU and for the IRU 600v3/v4 EHP RFU, which areadditionally powered using a separate DC input on their front panel, refer toPower Supply Connection on page 95 for DC power installation.Figure 37. IRU 600 and INUFigure 38. IRU 600v2 Tx Switch and RFUv2 Connections92 JULY 2018 AVIAT NETWORKS
IRU 600 INSTALLATION CHAPTER 5Figure 39. IRU 600v3/v4 Tx Switch and RFUv3 ConnectionsCAUTION: Ambient temperatures must not exceed 550C (1310F). If installed in a rack cabinet, it isthe ambient within the cabinet.Chassis GroundingThe chassis grounding stud accommodates ground cables up to 16 mm2(AWG 6).The stud also provides jack plug connection for a wrist strap.lGround the IRU 600 from the grounding stud to the rack/frame ground bar using4 mm2(AWG 12) green PVC insulated stranded copper wire with a suitably sizedcrimp lug at the ground bar end (supplied by the installer). For NEBS groundingcompliance, see below.lIf the equipment rack/frame requires grounding, use 16 mm2(AWG 6) wirefrom its ground bar to the station ground.NEBS Compliant GroundingThese grounding requirements apply for a NEBS compliant installation.lGround the IRU 600 from the grounding stud to the rack/frame ground bar using16 mm2 (AWG 6) green PVC insulated stranded copper ground wire (not 4 mm2)together with a star washer under the grounding screw at the ground-bar end.Torque the grounding post screw to 1.2-1.5 Nm (10-13 in-lbs).lCoat all bare conductors with an appropriate antioxidant compound beforecrimp connectors are fitted.lEnsure all unplated connectors, braided strap, and bus bars are brought to abright finish and then coated with an antioxidant before they are connected. Thisdoes not apply to tinned, solder-plated, or silver-plated connectors and otherplated connection surfaces – but all must be clean and free of contaminants.AVIAT NETWORKS JULY 2018 93
CHAPTER 5IRU 600 INSTALLATIONlWhere metallic raceway fittings are installed ensure all fittings are tightened toprovide a permanent low-impedance path.Safety Requirements for Equipment GroundinglDo not assume that an existing rack or mounting frame is correctly grounded.Always check the integrity of the ground connections, which must include a checkthrough to the master ground for the station, which should be located at the pointof cable entry to the equipment building. Ground wires must provide a direct, lowimpedance path to the master ground bar.lDo not connect other equipment to the same grounding cable as the INU. Eachitem of equipment in a rack must be separately grounded to the rack ground bar.lThe INU / IRU 600 must be located in the same immediate area (adjacentracks/cabinets) as all other equipment with a (ground) connection to a commonDC supply source.lAll intra-building signal cabling must be shielded, and both ends of each shieldmust be grounded.lThere must be no switching or disconnecting devices in the grounded circuitconductor between the DC source and the point of connection of the groundingelectrode conductor.Waveguide InstallationFor instructions on waveguide installation and associated pressurization and groundingrequirements, refer to the relevant documentation from the waveguide supplier. Generalguidance can be found in Aviat Networks Best Practices Guide.Waveguide Connection to ACUConnect ACU antenna port(s) to waveguide(s) using flexible waveguide.lInformation on required waveguide flanges and recommended waveguide typesare listed in the following table.lRemove and discard any protective flange/port covers before installation.94 JULY 2018 AVIAT NETWORKS
IRU 600 INSTALLATION CHAPTER 5Figure 40. ACU and Waveguide ConnectionTable 7. ACU Flange DataFreq, GHz Flange Type Holes Screw Length Waveguide5.8/6 CPR 137 G 8 x #10-32 tapped holes 1/2" WR 137* The screw length assumes a flex twist mating flange thickness of 1/4”.Power Supply ConnectionNOTE: The DC power supply must be SELV compliant (maximum limited60 Vdc).For IRU 600 power consumption figures refer to INU Power Supply on page 103.Power Supply RequirementsRFUs not fitted with a front-panel D-Sub M/F 2W2 power connector are powered via the IFcable from their associated INU/INUe. These are:lStandard power IRU 600(v1) and IRU 600v2 RFUslStandard/High power IRU 600v3/v4 RFUsRFUs fitted with a front-panel D-Sub M/F 2W2 power connector are additionally powered bya front panel connector. These are:AVIAT NETWORKS JULY 2018 95
CHAPTER 5IRU 600 INSTALLATIONlHigh power IRU 600(v1) and IRU 600v2 RFUslExtra high-power (EHP) IRU 600v3/v4 RFUslThe power connector and cable are identical to that used for the INU/INUe.-48 Vdc and +24 Vdc OperationThe associated INU/INUe requires a -48Vdc power input. For operation from a +24 Vdcpower supply a +24 to -48 Vdc converter is required.lThe plug-in PCC (Power Converter Card) can be installed to convert +24 Vdc to -48Vdc for connection to the -48 Vdc connector on the NCC. Two PCCs are required ifan NPC is also installed.oA PCC supports power consumption for the INU/INUe plus a maximum ofthree V1 or V2 RFUs, or a maximum of two V3/V4 RFUs. See PCC +24 VdcOperation on page 1lOtherwise a suitable external converter can be used - contact Aviat Networks fordetails.RFUs fitted with the front-panel D-Sub M/F 2W2 power connector support a wide-mouth +/-21 to 60 Vdc connection.lBoth +ve and -ve pins are isolated from ground. They can be powered from +24Vdc or -48 Vdc supplies.lThe integral DC/DC converter provides polarity protection, under/over voltageshutdown, over-current limit, and thermal shutdown. There are no serviceablefuses.lRun the supplied power cable through to a dedicated circuit breaker on the rackpower connect panel.oFor a -48 Vdc supply, connect the blue wire to -48 Vdc (live), and the black wireto ground/+ve. The circuit breaker should have rating of 3 A.oFor a +24 Vdc supply, connect the blue wire to +24 Vdc (live), and the blackwire to ground/-ve. The circuit breaker should have rating of 5 A.oFor NEBS compliance the battery return connection is to be treated as anisolated DC return (DC-I), as defined in GR-1089-CORE.CAUTION: Use the RFU circuit breaker as the power connect/disconnect device - do notuse the front-panel 2W2 DC connector for live power connect/disconnect.IRU 600(v1) and IRU 600v2Standard power RFUs are powered over the IF cable from its INU/INUe.High power RFUs (HP) are additionally powered using a separate DC input on their frontpanel.IRU 600v3lThe Std/HP RFU is powered over the IF cable from its INU/INUe.oThe RFU is SW configured for standard or high-power. High power operation96 JULY 2018 AVIAT NETWORKS
IRU 600 INSTALLATION CHAPTER 5requires installation of a feature license (EZF-61 to 66, or EZG-61 to 66).lA feature license is not required for the EHP RFU.Insertion Loss LabelsLabels on the ACU provide factory-measured insertion loss data. These list the loss foreach filter and circulator, and the total loss through the ACU (filters, circulators, cables,plus any protection components, such as Tx switch and couplers). Total (combined) lossfigures are entered into Portal to enable computation of Tx power and RSL figures at theACU antenna waveguide port(s) based on the RFU measured values of Tx power and RSL.For IRU 600v2 and IRU 600v3/v4 an additional label shows the insertion loss of the Txmonitoring port. The value must be considered when measuring output power with a powermeter.Expansion Port UseThe expansion port allows system expansion through the addition of co-located IRU 600radios, or external radio equipment.When multiple carriers are deployed on a common branching network (same antenna), theselection and installation of branching network components must be such that thresholddegradation caused by intermodulation products is avoided.lWhile the IRU 600 ACUs are specified to avoid placing undue constraints onfrequency planning for multiple carrier systems, the following conditionalrequirements are intended to provide guidelines on the selection and installationof branching frequencies and components.oThe intermodulation frequency products that result from combining two ormore transmitter frequencies on a common antenna feeder should be 48 MHzor more above or below each of the receiver frequencies present on the sameantenna feeder.oSystems employing carrier frequencies with potential to causeintermodulation products within 48 MHz of any of the receiver frequenciespresent on the same antenna branching network (feeder) must be designedand installed to mitigate the effects of such intermodulation products.FAN ModuleThe fan units in an RFU are removable for service/replacement. Fan module replacementis non-traffic affecting.CAUTION: Fan module hazard - keep away from moving fan blades.AVIAT NETWORKS JULY 2018 97
CHAPTER 5IRU 600 INSTALLATIONCAUTION: Handle the FAN module with care. Do not physically shock the module or touchthe fan impeller blades. Doing so can move the impeller off-center and cause prematurefan failure.lFor IRU 600(v1) and IRU 600v2 a fan cover is removed to expose the two fans.Removal and replacement is per-fan.lFor the IRU 600v3 the four fans are located on a removable/replaceable front-cover fan tray.oTo remove, unscrew the fan tray fasteners, ease outwards, and carefully dis-connect the rear cable connector. Fan replacement is per-tray.oWhen replacing the fan tray ensure the supply cable is routed so it is not pinchedwhen the tray is fastened, and that during operation it cannot come into contactwith a fan.lFan operation is monitored. Each fan has a matching alarm.lFor IRU 600(v1) and IRU 600v2 both fans are operated at a fixed speed.lIRU 600v3 fan speed is temperature-dependent.NOTE: If one fan needs to be replaced, replace all fans.Figure 41. IRU 600v3 Fan Tray RemovalChassis Adapter Kit for IRU 600v3 and IRU 600v4RFUsAn adaptor kit (part No. 179-530112-002) is available to enable installation of an IRU 600v3RFU into an IRU 600v2 or IRU 600v1 chassis.Aadaptor kits to enable installation into an IRU 600v2 or IRU 600v1 chassis are as follows:l(Part No. 179-530112-002) is available to enable installation for an IRU 600v3RFU, andl(Part No. 179-530508-001) for an IRU 600v4 RFU.98 JULY 2018 AVIAT NETWORKS
IRU 600 INSTALLATION CHAPTER 5The kit is used where an existing V2 or V1 chassis is to be upgraded to V3/V4 capabilities –the existing V2 or V1 RFU is replaced by a V3/V4 Std/HP RFU, or EHP RFU.One kit is required per IRU 600v3/v4 RFU.NOTE: For the IRU 600v3 or v4 to be recognized the installed Eclipse SWmust be 07.03.56, or later compatible release.The kit, comprises:lA riser plate that properly locates the physically smaller IRU 600v3/v4 RFUwithin the V2 or V1 chassis.lExtension plate for the V3 or V4 Fan Tray to provide a neat and integratedappearance in its V2 or V1 host chassis. The extension plate is designed for usewith all V3 or V4 Fan Tray types.lVarious screws and an overlay to mask an unused screw hole.lInstallation instructions.NOTE:lWhere the V3 or V4 Std/HP RFU is installed an HP feature license (EZF-61 to 66,or EZG-61 to 66) must be installed to enable the HP option.lWhere the V3 or V4 EHP RFU is installed a feature license is not required – theEHP capability is inclusive.lWhere a V3 or V4 RFU (or V2) RFU is used in a system with a V1 ACU, the 'MuteOffline Tx Power' tab on the IRU 600v3/v4 (or IRU 600v2) plug-ins RAC/RFUscreen may be retained until Break/Create protection is toggled. In the Protectionscreen, break protection and click Send, followed by create protection and Send,after which the 'Mute Offline Tx Power' tab will be removed to reflect that it isoperating in a V1 environment.For information on V4, V3, V2, V1 compatibility see IRU 600 Compatibility on page 72.ProcedurelInstall the adapter kit on the V3 or V4 RFU according to the adapter kitinstruction sheet.lIf the V3 or V4 RFU is Std/HP and the HP capability is required, install therelevant HP feature license. (A feature license is not required for the EHP RFU).lInstall the V3 or V4 RFU in the IRU 600 V1 or V2 chassis according to theinstruction sheet.lFor the V3 or V4 EHP RFU install the supplied DC power cable. Ensure it isterminated onto a correctly sized circuit breaker. See Power Supply Connectionon page 95.lConfigure the IRU 600 with V3 or V4 RFU according to the instructions providedin the Portal Chapter of this manual. See Configuration Procedures for RAC70/7X, RAC 60/6X and RAC 60E/6XE on page 1.AVIAT NETWORKS JULY 2018 99
CHAPTER 5IRU 600 INSTALLATIONNext StepslINU/INUe installation. Refer to Installing the INU and INUe on page 101.100 JULY 2018 AVIAT NETWORKS
INSTALLING THE INU AND INUE CHAPTER 6Chapter 6. Installing the INU and INUeThe INU and the INUe are the indoor units for the Eclipse Node.This chapter includes:lINU/INUe Description on page 102lCompact Flash Card on page 1lINU/INUe Installation Requirements on page 115lInstallation on page 118lPlug-in Slot ConfigurationlPlug-in Installation Requirements on page 121For a description of the plug-ins, refer to the Eclipse Platform Product Description.For information on user-interface connector and cable data, refer to INU/INUe and IDUConnector and Cable Data on page 1.CAUTION: With the increase in the capabilities and complexity of some new plug-inmodules, such as RAC 60E, RAC 6XE, DAC GE3, Compact Flash cards with increasedcapacity are required. See Compact Flash Card on page 1.CAUTION: Do not turn power off within 10 minutes of initial INU/INUe turn-on, or initialturn-on after a new compact flash card is installed.CAUTION: There must be a minimum of 50 mm (2”) of side spacing from the INU/INUe toany rack panels, cable bundles or similar, and 50 mm (2”) of space to the front and backof the RF section to ensure proper ventilation.AVIAT NETWORKS JULY 2018 101
CHAPTER 6INSTALLING THE INU AND INUEINU/INUe DescriptionThe INU/INUe is a rack-mounted unit that pairs with one or more ODUs or one or more IRU600s to make an Eclipse Node.An INU/INUe comprises a chassis (IDC/IDCe) and plug-ins.The IDC/IDCe has dedicated slots for the NCC and FAN plug-ins, and either four slots (IDC)or ten slots (IDCe) available for optional RAC, DAC, AUX and NPC plug-ins.Refer to:lIDC V1 and IDC V2 and INU Front PanelLayout in this sectionlFAN Air Filter Option on page 113lPower Line Filter Option on page 114lPlug-in Slot Configuration on page 1INU Front Panel LayoutThis figure is an example of an INU front panel, with one DAC x16, two RAC30s, and ablanking panel over the unused slot. For a full description of all plug-ins and their frontpanel layouts, refer to the Eclipse System Description.Figure 42. Typical INU Front Panel LayoutNo Item/Label Description1Rack Ear andgrounding studRack attachment bracket for the IDC. One ear has a combined ESD andIDC grounding stud. The ears can be fitted either side, which provideflush-with-rack-front mounting.2RAC 30 RAC 30 fitted in slot 13NCC Mandatory Node Control Card (dedicated slot)4Blank Panel Blanking panel fitted to slot 25RAC 30 RAC 30 fitted in slot 4102 JULY 2018 AVIAT NETWORKS
INSTALLING THE INU AND INUE CHAPTER 6No Item/Label Description6DAC 16x 16xE1/DS1 DAC fitted in slot 37FAN Mandatory fan plug-in (dedicated slot)INU Power SupplyINUs require a -48Vdc power supply (+ve earth) but will operate to specification over avoltage range of -40.5 to -60Vdc.The return (+ve) pin on the NCC and NPC power supply connectors is clamped to chassisground via polarity-protecting power FETs.lNCC and NPC power inputs are reverse polarity protected (the input fuse will notblow if polarity is reversed).For NEBS compliance the battery return connection is to be treated as a common DC return(DC-C), as defined in GR-1089-CORE.Where operation from a +24 Vdc PSU is required, the plug-in PCC option provides voltageconversion from + 24 (19 to 36) Vdc to -56 Vdc for connection to the NCC -48Vdc input. -56Vdc represents a typical (maximum) float voltage for a battery-backed -48 Vdc supply.Otherwise an external +24 to -48 Vdc converter can be used - contact Aviat Networks fordetails.The dc power supply must be UL or IEC compliant for SELV (Safety Extra Low Voltage)output (60Vdc maximum limited).Voltage changes due to the regulation of the power supply must not exceed a change-rate(linear variation slope) of 7 V/ms, as specified in TSI EN 300 132-2 V2.4.6. Applies overvariations between -40.5 Vdc to -57 Vdc.Power Consumption and INU Load MaximumsTotal power consumed is dependent on the number and type of plug-in cards, the numberand type of ODU(s) or IRU 600, plus for the ODUs, the frequency band.INU loading maximums, the number and type of RACs and DACs that can be installed in anINU, are determined by the load capacity and temperature limits of the DC converter in theNCC and NPC, which supply various DC rails to the plug-in cards. Load maximums are alsodependent on the SW release in use, and the version of NCC and NPC installed. For moreinformation see Node Card Maximums below.lODUs, IRU 600s and FANs are not powered via the NCC converter, meaning theODU and IRU 600 type does not impact INU link loading. Their DC supply is takenfrom the -48 Vdc power supply input connector.lHowever, if a PCC is installed for +24 Vdc operation, the INU cards and associatedODUs or IRU 600s are supplied from the PCC, meaning PCC power limits areAVIAT NETWORKS JULY 2018 103
CHAPTER 6INSTALLING THE INU AND INUEdetermined by the INU cards and by the number and type of ODUs or IRU 600sfitted.lA PCC should always be installed to receive maximum FAN cooling. This means itshould be installed in the immediate FAN-side slots in an INU/INUe.NOTE: A suitable external +24 Vdc to -48 Vdc converter can be usedinstead of the PCC. Contact Aviat Networks for details.Power ConsumptionPower consumption figures are for a -48 Vdc supply voltage at normal room ambients.Plug-in CardsThe table below lists nominal power consumption figures for Eclipse plug-ins.lUse these together with the ODU or IRU600 consumption figures in the followingtables to determine total nodal power consumption.lWhen operated with an ODU, cable power dissipation should be considered.Table 8. Typical Plug-in Power ConsumptionsItem Consumption WRAC30v3, RAC 30A 8RAC40 10RAC 4X 15RAC 3x 11RAC 60/60E 12RAC 6X/6XE 17RAC 70 13DAC ES, 16x, 16xV2, 4x, 3xE3/DS3, 3xE3/DS3M 2.5DAC GE, 155o, 2x155o, 2x155e, 155oM, 155eM 4DAC GE3 13NCM 10NCC 11NPC 8AUX 1FAN 1RU* 2FAN 2RU* 2* FANs are not powered via the NCC/NPC converter.104 JULY 2018 AVIAT NETWORKS
INSTALLING THE INU AND INUE CHAPTER 6IRU 600(v1) and IRU 600v2The table below lists nominal figures.lFor a standard power RFU, DC power is provided from its INU/INUe via its RAC -RFU cable (in the same way as an ODU).lFor a high-power RFU, power is supplied via its RAC cable and additionally by afront-mounted DC connector to an external DC power source. High power isenabled through feature licensing. See Licensing on page 1.Table 9. Typical IRU 600(v1) and IRU 600v2 Power ConsumptionConfiguration Band PowerSourcedfrom INUPower Sourcedfrom ExternalDC ConnectorTotal DCPower1+0 Configurations Std Power – Normal Operation L6/U6 52W N/A 52W1+0 Configurations Std Power –All Tx Muted L6/U6 30W N/A 30W1+0 Configurations High-Power – Normal Operation 5.8/L6/U6/7/8/10/1152W 38W 90W4GHz N/A 80W 80W1+0 Configurations High-Power – All Tx Muted 5.8/L6/U6/7/8/10/1130W 4W 34W4GHz N/A 25W 25W1+1 Configurations Std Power – Normal Operation L6/U6 82W N/A 82W1+1 Configurations Std Power – All Tx Muted L6/U6 60W N/A 60W1+1 Configurations High-Power – Normal Operation 5.8/L6/U6/7/8/10/1182W 42W 124W4GHz N/A 105W 105W1+1 Configurations High-Power – All Tx Muted 5.8/L6/U6/7/8/10/1160W 8W 68W4GHz N/A 50W 50W1+1 Configurations employing FD Std Power – NormalOperationL6/U6 104W N/A 104W1+1 Configurations employing FD Std Power – All TxMutedL6/U6 60W N/A 60W1+1 Configurations employing FD High-Power –Normal Operation5.8/L6/U6/7/8/10/11104W 76W 180W4GHz N/A 160W 160WAVIAT NETWORKS JULY 2018 105
CHAPTER 6INSTALLING THE INU AND INUEConfiguration Band PowerSourcedfrom INUPower Sourcedfrom ExternalDC ConnectorTotal DCPower566651+1 Configurations employing FD High-Power –All Tx Muted5.8/L6/U6/7/8/10/1160W 8W 68W4GHz N/A 50W 50W1+1 Configurations Std Power – MHSB (IRU 600v2Only)L6/U6 104W N/A 104W1+1 Configurations High-Power – MHSB (IRU600v2Only)5.8/L6/U6/7/8/10/11104W 76W 180W4GHz N/A 160W 160W1+1 Configurations Std Power – MHSB (IRU 600v2Only)L6/U6 82W (avg)104W(peak)N/A 82W(avg)104W(peak)1+1 Configurations High-Power – MHSB (IRU600v2Only)5.8/L6/U6/7/8/10/1182W (avg)104W(peak)42W (avg)76W (peak)124W(avg)180W(peak)4GHz N/A 105W (avg)160W (peak)105W(avg)160W(peak)IRU 600v3The table below lists typical and maximum power consumption figures at maximum Txpower settings.lA common RFU is used for standard (SP) and high-power (HP) modes. Highpower is enabled through feature license. See Licensing on page 1.oFor both standard power and high-power operation DC power to the RFU(s) isprovided from its INU/INUe via the RAC - RFU cable.lThe EHP RFU power is supplied via its INU/INUe RAC cable and additionally by afront-mounted DC connector to an external DC power source.Table 10. Typical and Maximum IRU 600v3 Power ConsumptionConfiguration TypicalINU/INUeSourcePwrMaxINU/INUeSourcePwrTypicalExternalDCSourcePwrMaxExternalDC SourcePwr1+0 Configurations IRU 600SPv3 – Normal Operation 58W 63W N/A N/A1+0 Configurations IRU 600SPv3 – All TX Muted 42.5W 46.5W N/A N/A106 JULY 2018 AVIAT NETWORKS
INSTALLING THE INU AND INUE CHAPTER 61+0 Configurations IRU 600HPv3 – Normal Operation 63W 68W N/A N/A1+0 Configurations IRU 600HPv3 – All TX Muted 42.5W 46.5W N/A N/A1+0 Configurations IRU 600EHPv3 L6 – NormalOperation58W 63W 56W 60W1+0 Configurations IRU 600EHPv3 U6 – NormalOperation61.5W 65.5W 60W 63.5W1+0 Configurations IRU 600EHPv3 11GHz – NormalOperation58W 63W 43W 46W1+0 Configurations IRU 600EHPv3 L6/U6/11– All TXMuted42.5W 46.5W 3.5W 4W1+1 Configurations IRU 600SPv3 – HSB Mode 100.5W 109.5W N/A N/A1+1 Configurations IRU 600SPv3 – All TX Muted 85W 93W N/A N/A1+1 Configurations IRU 600HPv3 – HSB Mode 105.5W 114.5W N/A N/A1+1 Configurations IRU 600HPv3 – All TX Muted 85W 93W N/A N/A1+1 Configurations IRU 600EHPv3 – L6 - HSB Mode 100.5W 109.5W 59.5W 64W1+1 Configurations IRU 600EHPv3 – U6 - HSB Mode 104W 112W 63.5W 67.5W1+1 Configurations IRU 600EHPv3 – 11 - HSB Mode 104W 112W 43W 46W1+1 Configurations IRU 600EHPv3 – L6 - All TX Muted 85W 93W 7W 8W1+1 Configurations IRU 600EHPv3 – U6 - All TXMuted85W 93W 7W 8W1+1 Configurations IRU 600EHPv3 – 11 - All TXMuted85W 93W 7W 8W1+1 FD Configurations IRU 600SPv3 – NormalOperation116W 126W N/A N/A1+1 FD Configurations IRU 600SPv3 – All TX Muted 85W 93W N/A N/A1+1 FD Configurations IRU 600HPv3 – NormalOperation126W 136W N/A N/A1+1 FD Configurations IRU 600HPv3 – All TX Muted 85W 93W N/A N/A1+1 FD Configurations IRU 600EHPv3 – L6 - NormalOperation116W 126W 112W 120W1+1 FD Configurations IRU 600EHPv3 – U6 - NormalOperation123W 131W 120W 127W1+1 FD Configurations IRU 600EHPv3 – 11GHz -Normal Operation116W 126W 86W 92W1+1 FD Configurations IRU 600EHPv3 L6/U6/11– AllTX Muted85W 93W 7W 8W1+1 Configurations IRU 600SPv3 – MHSB Mode 116W 126W N/A N/A1+1 Configurations IRU 600HPv3 – MHSB Mode 126W 136W N/A N/A1+1 Configurations IRU 600EHPv3 – L6-MHSB Mode 116W 126W 112W 120W1+1 Configurations IRU 600EHPv3 – U6-MHSB Mode 123W 131W 120W 127W1+1 Configurations IRU 600EHPv3 – 11-MHSB Mode 116W 126W 86W 92W1+1 Configurations IRU 600SPv3 – P-MHSB Mode 100.5WAvg116W Peak109.5WAvg126W PeakN/A N/AAVIAT NETWORKS JULY 2018 107
CHAPTER 6INSTALLING THE INU AND INUE1+1 Configurations IRU 600HPv3 – P-MHSB Mode 105.5WAvg126W Peak114.5WAvg136W PeakN/A N/A1+1 Configurations IRU 600EHPv3 –L6 - P-MHSBMode100.5WAvg116W Peak109.5WAvg126W Peak59.5W Avg112W Peak64W Avg120W Peak1+1 Configurations IRU 600EHPv3 –U6 - P-MHSBMode104W Avg123W Peak112W Avg131W Peak63.5W Avg120W Peak67.5W Avg127W Peak1+1 Configurations IRU 600EHPv3 –11 - P-MHSBMode100.5WAvg116W Peak109.5WAvg126W Peak46.5W Avg86W Peak50W Avg92W PeakIRU 600v4The table below lists maximum power consumption figures at maximum Tx power settings.lA common RFU is used for standard (SP) and high-power (HP) modes. Highpower is enabled through feature license.lFor both SP and HP operation, DC power to the RFU(s) is provided from itsINU/INUe via the RAC - RFU cable.lThe EHP RFU power is supplied via its INU/INUe RAC cable and additionally by afront-mounted DC connector to an external DC power source.Table 11. Maximum Power Consumption (W) - IRU 600v4 with RAC 70Maximum Output Power (dBm)SP/HP Configuration,1+0 unit (Typical)31.5 27.0 22.0 Tx Muted11 GHz 64.3 47.5 39.8 23NOTE:lFor an EHP Configuration, 1+0 unit, the Maximum Power Consumptionis 100 W.lTX power values at RFM port, under ambient temperature of +30 °C.lTX power level shown is referenced at the 1+0 ACU antenna port.lThe power consumption is channel bandwidth independent and is thesame for any given TX power.lThe delta between TX output power at 1+0 ACU antenna port and theRFM port is the 1+0 ACU loss. For 11 GHz, ACU loss is 2.0 dB.Node Card MaximumsFrom SW release 5.04 improvements in the cooling fan operating logic allow higher cardloadings coupled with maximum ambients to 55oC (131oF), or 45oC (113oF).lFrom software release 5.04 fan logic improvements allow higher INUe loadingwhen an NPC is installed.lAn NPC must be fitted in an INUe where specified below. The NPC provides power108 JULY 2018 AVIAT NETWORKS
INSTALLING THE INU AND INUE CHAPTER 6supply load sharing with the NCC, allowing the overall loading to be increased.Should the NPC fail, airflow from the 2RU FAN is increased to compensate.lExtended FAN failure/impairment detection is included. For example, an alarmwill be raised on a reduction in fan speed (RPM), such as can occur as a result ofbearing wear/friction.lThe loading maximums are designed to ensure systems will continue to operatecorrectly in the event of failure of either the NCC or NPC.From November 2012 new card maximums (loading rules) apply with the availability ofupdated high-output NCC and NPC cards. These new cards have part numbers of EXN-003and EXS-002 respectively.lThe updated NCC and NPC cards are required where node loading exceeds 120W.lThe prior NCC and NPC cards, those with part numbers EXN-002 and EXS-001respectively, must only be retained where node loadings do not exceed 120W.CAUTION: When planning the number and type of cards to be installed in an INUe or INU,the following rules must be observed. These rules apply retrospectively (back tosoftware release 5.04).CAUTION: The loading rules below must be observed by the installer - there is no built-inmechanism to report or limit an incorrect dimensioning of power supply consumption.INUe Loading Rules for Operation up to 55ºC (131ºF)The following loading rules must be followed when dimensioning the total powerconsumption of an INUe that is required to operate in ambient temperatures up to 55ºC(131ºF):lIf the total power consumption of all cards installed exceeds 85W, an NPC mustbe fitted, a 2RU FAN card must be fitted, and 5.04 or later SW loaded.lWith this configuration confirmed (NPC + 2RU FAN + 5.04 SW or later) themaximum INUe loading enabled is:o120W with NCC EXN-002 and NPC EXS-001.o125W with high-output NCC EXN-003 and NPC EXS-002.oThe installed total of DAC GE3 cards must not exceed four.lIf an earlier version of SW is loaded, the maximum INUe loading allowed is 85Watts. This applies whether or not an NPC and 2RU FAN are fitted.CAUTION: 55ºC (131ºF) operation does not apply to the PCC. Operational ambienttemperatures with a PCC installed must not exceed 450C (1130F).Install a suitable external +24 Vdc to -48 Vdc converter to avoid the PCCoperational ambient temperature limits. Contact Aviat Networks for details.AVIAT NETWORKS JULY 2018 109
CHAPTER 6INSTALLING THE INU AND INUEINUe Loading Rules for Operation up to 45ºC (113ºF)The following loading rules must be followed when dimensioning the total powerconsumption of an INUe that is operating in ambient temperatures that do not exceed 45ºC(113ºF):lIf the total power consumption of all cards installed exceeds 85W, an NPC mustbe fitted, a 2RU FAN card must be fitted, and 5.04 or later SW loaded.lWith this configuration confirmed (NPC + 2RU FAN + 5.04 SW or later) themaximum INUe loading enabled is:o120W with NCC EXN-002 and NPC EXS-001.o146W with high-output NCC EXN-003 and NPC EXS-002.oThe installed total of DAC GE3 cards must not exceed four.lIf an earlier version of SW is loaded, the maximum INUe loading permitted is100W. This applies whether or not an NPC and 2RU FAN are fitted.Typical compliant loading examples are shown below with 5.04 SW or later (48Vdc powersource).Table 12. NCC EXN-002 with EXS-001, 45ºC (113ºF)Total Watts: 119 118 120 120Qty RAC 60E 6 0 0 6Qty RAC 6x 0 4 4 0Qty DAC 16xV2 0 1 2 0Qty AUX 0 1 0 1Qty NPC 1 1 1 1Qty NCC 1 1 1 1Qty FAN 1 1 1 1Qty DAC GE3 2 2 2 2Table 13. NCC EXN-003 with EXS-002, 45ºC (113ºF)Total Watts 139 135 132 146Qty RAC 60E 2 4 4 0Qty RAC 6XE 4 2 0 4Qty DAC 16xV2 0 2 4 2Qty AUX 0 1 1 0Qty NPC 1 1 1 1Qty NCC 1 1 1 1Qty FAN 1 1 1 1Qty DAC GE3 2 2 4 4INU Loading RulesThe INU (1RU) chassis should not be loaded above the follow limits:l65 watts total for operation up to 45ºCl50 watts total for operation up to 55ºC110 JULY 2018 AVIAT NETWORKS
INSTALLING THE INU AND INUE CHAPTER 6lA maximum of two DAC GE3 cards.No improvements are introduced for the INU with 5.04 SW due to its use of smaller, lowervolume cooling fans.NOTE: Elevated ambient temperatures should be avoided. The ambienttemperature is the air temperature in the immediate operatingenvironment of the chassis, which if installed in a rack, is the ambientapplying to its location within the rack.CAUTION: The ambient temperature maximums must not be exceeded. Over-temperature operation is a primary factor affecting long term component reliability.PCC +24 Vdc OperationThe PCC is for use with standard +24 Vdc (-ve grounded) battery-backed power supplysystems.lOne PCC supports:oUp to 200W in air-conditioned installations (ambient max 250C / 770F)oUp to 150W in non-air-conditioned installations (ambient max 450C / 113oF).oRefer to power consumption figures above to determine a load maximum for aparticular configuration.lThe PCC +ve and -ve input terminals are isolated from chassis (ground). The -veinput is grounded by the -ve grounded power supply connection.lThe PCC 20A fuse is fitted in the +ve input. It is a PCB mount type and is not fieldreplaceable.lReverse polarity protection is provided. The PCC will automatically recover froma reverse polarity connection - the fuse will not blow. Over temperature thermalprotection is included.lThe PCC conversion efficiency is nominally 10%. To determine the powerconsumed by the PCC, use a figure of 10% of the power consumed by theINU/INUe cards and RFUs (ODU / IRU 600).lWhen installed in an INUe the INUe must be fitted with the 2RU FAN module as itprovides almost double the air flow of the 1RU FAN modules.lThe PCC must be connected to the NCC before applying power to the PCC to avoida current-inrush trip (overload) on the PCC.lThe PCC can be plugged into any INU/INUe option slot. It is not connected to thebackplane and its function is not monitored within Portal.oThe PCC should be installed next to the FAN card to get best air-flow cooling.lWhere an NPC is fitted, two PCCs are required for +24 Vdc operation, one for theNCC, the other for the NPC. This means an INUe must be used for NCC + NPCAVIAT NETWORKS JULY 2018 111
CHAPTER 6INSTALLING THE INU AND INUEoperation.lIf the PCC front-panel LED is not lit, it indicates the existence of abnormalconditions such as output under-voltage, output over-voltage, loss of input power,output over-current, or open input fuse.NOTE: The PCC function can be replaced by a suitable external +24 Vdc to-48 Vdc converter. Contact Aviat Networks for details.Power CablesThe INU power cable is supplied in the IDC Installation Kit. It is supplied with a D-sub M/F2W2 connector fitted at one end and wire at the other. The cable is nominally 5m (16ft), andthe wires are 4mm2 (AWG12).The cable is used for -48 Vdc connections to an NCC or NPC, or for +24 Vdc connections to aPCC.The blue wire must be connected to live (-48 Vdc or +24 Vdc); the black wire to ground (+48Vdc or -24 Vdc).Figure 43. Power Cable and ConnectorCAUTION: Use the INU circuit breaker as the power connect/disconnect device - do notuse the front-panel 2W2 DC connector for live power connect/disconnect.The PCC is supplied with a power cable to connect to an NCC or NPC.Similarly, the optional NEBS power line filter unit is supplied with a power cable to connectto an NCC, NPC, or PCC.This cable is fitted with a D-sub M/F 2W2 connector at each end. Note that a standard powercable is not included for the reason the cable supplied with an NCC (or NPC) is not usedwhen powered from a PCC, or via a power line filter, so the cable is re-used as the powerinput cable for the PCC or filter unit.112 JULY 2018 AVIAT NETWORKS
INSTALLING THE INU AND INUE CHAPTER 6FusesThe NCC and NPC are fitted with a fast-acting 25A fuse fitted on the PCB behind the powercable connector. (Early production NCCs were fitted with a front panel fuse/switch with a12.5A slow-blow fuse).The PCC is fitted with a fast-acting PCB-mounted 20A fuse.NCC, NPC and PCC fuses are not field-replaceable.FAN Air Filter OptionA fan air filter option is available for installation with the FAN module in an INU, and with the2RU FAN module in an INUe. Where Eclipse is required to be NEBS (Network Equipment-Building System) compliant, the fan air filter must be installed.NOTE: The fan air filter must be inspected regularly and replaced whendust laden. In normal telecommunications equipment-roomenvironments inspection must be at not more than 12 monthly intervals.In other environments where air quality is not controlled, more frequentinspection is required.CAUTION: A heavily dust-laden filter will severely restrict fan air flow and may lead toover-heating.NOTE: Excessive heat is the number one cause of premature equipmentaging and failure.To maximize long term component reliability, the fan air filter must notbe allowed to become clogged, and ambient temperature limits must notbe exceeded.Fan Air Filter InstallationFor the INUe a fan air filter kit is supplied, comprising a filter frame, filter element, andfastening screw. For the INU the filter it is a single-piece element. It is installed in theINU/INUe to the right side of the FAN module, as illustrated below for an INUe.Remove the FAN module and slide the air filter into the chassis so that it locates to the rightside of the FAN module backplane connector, and up against the chassis side. FAN moduleremoval and replacement does not affect traffic.Installation instructions are included with the fan filter kit.AVIAT NETWORKS JULY 2018 113
CHAPTER 6INSTALLING THE INU AND INUEFigure 44. Location of Fan Air Filter in INUePower Line Filter OptionAn external DC power line filter option is available and must be installed with an INU/INUefor NEBS compliance. It ensures Eclipse meets EMI requirements specified withinTelcordia GR-1089-CORE, Issue 4, June 2006.It is IRU tall and 140 mm wide (5.5”) and is supplied as a kitset comprising the filter unit,bracket for left or right-side rack mounting, and a short 2W2 to 2W2 cable for connectingthe filter unit to the NCC or NPC -48 Vdc inputs.Where an NPC is fitted, two filter units are required, one for the NCC, the other for theNPC.The standard power cable supplied with an INU or NPC is re-used as the power inputcable for the filter unit.Figure 45. Power Line Filter with Bracket114 JULY 2018 AVIAT NETWORKS
INSTALLING THE INU AND INUE CHAPTER 6INU/INUe Installation RequirementsTable 14. INU/INUe Installation RequirementsFunction/Requirement Priority DetailsRestricted access The INU/INUe and its associated dc power supply must be installed in arestricted access area such as a secure equipment room, closet, or cabinet.For NEBS compliance this equates to installation of the INU/INUe in a secure,restricted access central office (CO) or customer premises (CP) location.Required Rack Space The INU requires 44.5mm (1RU) of vertical rack space and 300mm rackdepth. The INUe requires 89mm (2RU) vertical rack space and 300mm rackdepth.Ventilation INU/INUe requires unobstructed air passage to each side for ventilationpurposes. There must be a minimum of 50mm (2”) of side spacing to any rackpanels, cable bundles or similar. No space above or below is required forventilation purposes.Maximum AmbientTemperatureThe INU/INUe is specified for a maximum ambient temperature (Tmra) of+55°Celsius (131° Fahrenheit). Conditions apply - see INU Power Supply onpage 103. The maximum ambient temperature (Tmra) applies to theimmediate operating environment of the INU, which if installed in a rack, is theambient applying to its location within the rack.Physical stability Ensure that adding an INU/INUe to a rack does not adversely impact thephysical stability of the rack.Power Supply -48 Vdc The INU/INUe PWR modules have the +ve pin on their dc power supplyconnector connected to the chassis.It must be used with a -48Vdc power supply which has a +ve ground; thepower supply ground conductor is the +ve supply to the INU.The power supply must have an accessible power disconnect device (mainswitch).Power Supply +24 Vdc A PCC is required to provide a +24 Vdc to -48 VDC conversion. The dc powersupply supplying the PCC must be -ve grounded.There must be no switching or disconnecting devices in the ground conductorbetween the dc power supply and the point of connection to a PCC.D.C. Supply Ground Con-nectionThe INU/INUe has a connection between the earthed conductor of the d.c.supply circuit and the earthing conductor.The INU/INUe must be connected directly to the d.c. supply system groundingelectrode conductor or to a bonding jumper from a grounding terminal bar orbus to which the d.c. supply system grounding electrode is connected.Switching or disconnecting devices must not be in the grounded circuitconductor between the d.c. source and the point of connection of thegrounding electrode conductor.AVIAT NETWORKS JULY 2018 115
CHAPTER 6INSTALLING THE INU AND INUEFunction/Requirement Priority DetailsEquipment Location INU/INUe must be located in the same immediate area (such as, adjacentcabinets) as any other equipment that has a connection between thegrounded conductor of the same d.c. supply circuit and the groundingconductor, and also the point of grounding of the d.c. system. The d.c. systemshall not be grounded elsewhere.Location of D.C. Power Sup-plyThe d.c. supply source for INU/INUe must be located within the samepremises as the INU/INUe.D.C. Supply Compliance,Loading and ProtectionThe dc power supply must be UL or IEC compliant for a SELV output (60Vdcmaximum).Check to ensure that connection of an INU/INUe to a new or existing dcsupply does not overload the supply, circuit protection devices and wiring.The INU/INUe and optional NPC module must each be supported from adedicated circuit breaker located on their rack power distribution panel.The circuit breaker(s) should have a rating of:12A for the INU, and for optional NPC25A for the INUe, and for optional NPC15A for the PCCThe circuit breaker(s) must be used as the INU/INUe powerconnect/disconnect devices - do not use the front panel connectors asconnect/disconnect devices.For NEBS compliance the battery return connection is to be treated as acommon DC return (DC-C), as defined in GR-1089-CORE.Cable routing INU/INUe Cat5, tributary, auxiliary and NMS cables are not to be routed withany AC mains power lines. They are also to be kept away from any powerlines which cross them.Chassis Grounding The INU/INUe chassis must be grounded to the station or master ground,which must be the same ground as used for the dc power supply. Normallythis is achieved by grounding the INU/INUe to the ground bar in its equipmentrack or frame. This bar is most often located to one side of the rack or at racktop or bottom. In turn, the ground bar is grounded to the station ground.Fan Air Filter The fan air filter must be installed where the INU/INUe is required to beNEBS compliant. The filter must be inspected regularly and replacedwhen dust laden. Inspection must be at not more than 12 monthly inter-vals in controlled air environments, or more frequently otherwise.Power Line Filter The power line filter must be installed where the INU/INUe is requiredto be NEBS compliant.Compact Flash CardCompatibilityWhere plug-in cards such as RAC 60E, RAC 6XE , DAC GE3, are to beinstalled into an existing INU, first ensure the Compact Flash card fittedin the NCC will support the required capacity. See Compact Flash Cardon page 1.NCC Compatibility Where a higher capacity Compact Flash Card is to be installed into an existingINU/NCC (NCC V2) to support RAC 60E, RAC 6XE, DAC GE3 operation, firstensure NCC compatibility with higher capacity Compact Flash cards. SeeCompact Flash Card on page 1.For information on NCC V1 / NCC V2 compatibility refer to Plug-in InstallationRequirements on page 121.116 JULY 2018 AVIAT NETWORKS
INSTALLING THE INU AND INUE CHAPTER 6Function/Requirement Priority DetailsIntrabuildinginterfaces and cabling(NEBS Compliance)Intrabuilding connections to/from Eclipse ports must only be connected viaintrabuilding or unexposed wiring or cabling.Intrabuilding ports MUST NOT be metallically connected to interfaces thatconnect to the OSP or its wiring. These interfaces are designed for use asintrabuilding interfaces only (Type 2 or Type 4 ports as described in GR-1089-CORE, Issue 4) and require isolation from the exposed OSP cabling. Theaddition of Primary Protectors is not sufficient protection in order to connectthese interfaces metallically to OSP wiring.Shielded and grounded cables must be used for intrabuilding cabling to/fromEclipse ports. Cables must be grounded at both ends.AVIAT NETWORKS JULY 2018 117
CHAPTER 6INSTALLING THE INU AND INUEInstallationProcedurelFit the rack mounting ears to the chassis with the grounding stud to left or rightside for the most direct ground wire path to the rack ground bar.lLocate the INU/INUe in the equipment rack and secure it using four No.12Phillips dome-head screws from the IDC installation kit.lGround the INU/INUe from the grounding stud to the rack/frame ground barusing a length of 4mm2 (AWG12) green PVC insulated stranded copper wirewith a suitably sized ground lug at the ground bar end (supplied by the installer).The grounding stud accommodates ground cables up to 16 mm2(AWG6). The stud also provides jack plug connection for a wrist strap.lIf the equipment rack/frame requires grounding, use 16mm2 (AWG6) wirefrom its ground bar to the station ground.Grounding Safety:oDo not assume that an existing rack or mounting frame is correctly grounded.Always check the integrity of the ground connections, which must include acheck through to the master ground for the station, which should be located atthe point of cable entry to the equipment building. Ground wires must provide adirect, low impedance path to the master ground bar.oDo not connect other equipment to the same grounding cable as the INU. Eachitem of equipment in a rack must be separately grounded to the rack groundbar.oThe INU must be located in the same immediate area (adjacentracks/cabinets) as all other equipment with a (ground) connection to acommon DC supply source.For NEBS compliance:oInstall the fan air filter option. Options are available for the IRU INU and IRUINUe. See FAN Air Filter Option on page 113.oInstall the NEBS power line filter unit. Install immediately below or above theINU. Separate filter units are required for the NCC and, where fitted, the NPC.Use the supplied 2w2 to 2w2 cable to connect the output of the filter unit to theinput of the NCC or NPC.oTo ground the INU use 16 mm2 (AWG 6) green PVC insulated stranded copperwire together with a star washer under the grounding screw at the ground-barend. Torque the INU grounding post screw to 1.2-1.5 Nm (10-13 in-lbs).118 JULY 2018 AVIAT NETWORKS
INSTALLING THE INU AND INUE CHAPTER 6oAll bare conductors must be coated with an appropriate antioxidant compoundbefore crimp connectors are fitted.oAll unplated connectors, braided strap, and bus bars must be brought to abright finish and then coated with an antioxidant before they are connected. Thisdoes not apply to tinned, solder-plated, or silver-plated connectors and otherplated connection surfaces – but all must be clean and free of contaminants.oAll raceway fittings must be tightened to provide a permanent low-impedancepath.lInstall the plug-ins in their assigned slot positions, and check that their frontpanels are flush-fitted (not protruding) and held secure by their fasteners.Ensure unused slots are covered by blanking panels. See See "Plug-in SlotConfiguration", and Plug-in Installation Requirements on page 121.oIf a FAN air filter is required, fit it prior to inserting the FAN.oInstall the CompactFlash card in the NCC; insert in the socket on the rightside of the PCB.lFor an ODU, fit the supplied jumper cable between the RAC and ODU cable, orwhere required to a lightning surge arrestor. See Arrestor Installation atBuilding Entry on page 1. Secure the cable within the rack/frame using cableties or similar. If the jumper cable is too short, make an extension cable. SeeJumper Cables on page 1.lFor an IRU 600, fit the supplied jumper cable between the RAC and companionIRU 600 RFU.lFit the DAC tributary cables. For information on the tributary cable sets, refer toSee "INU/INUe and IDU Connector and Cable Data"NOTE: For a DAC 16x, ensure correct orientation of the Mini RJ-21connector before pushing it home. This can be checked by the scallopedkey to one side of the connector. Additionally, a tributary cable suppliedby Aviat Networks will have the cable exiting to the right side whenviewed from the front. Do NOT over-tighten the Mini RJ-21 retainingscrews.The following steps describe the procedure for installing the power cable and preparing forpower-on. Do not connect the power until all steps have been completed.lRun the supplied power cable through to the power pick up point, which willnormally be at a circuit breaker panel in the rack. A circuit breaker (or fuse)should have a capacity of 12A for the INU and a 25A for the INUe, howeverthese ratings can be adjusted in line with the number of cards installed, andhence power consumption. For power consumption data, see INU PowerSupply on page 103.lFor a -48 Vdc supply, connect the blue wire to -48Vdc (live), and the black wireto ground/+ve. (Power input on the NCC and NPC is polarity protected).lFor a +24 Vdc supply, connect the blue wire to +24Vdc (live), and the black wireAVIAT NETWORKS JULY 2018 119
CHAPTER 6INSTALLING THE INU AND INUEto ground/-ve. (Power input on the PCC is polarity protected).lMeasure the voltage on the dc power connector.oFor -48 Vdc operation the voltage should be -48Vdc, +/-2Vdc for a non-batteryfloated supply, and nominally -56 Vdc for a battery floated supply. (Limits are -40.5 to - 60 Vdc).oFor +24 Vdc operation the voltage should be 24 +/- 2Vdc for a non-batteryfloated supply, and nominally 30 Vdc for a battery floated supply. (Operatinglimits are 20 to 36 Vdc).NOTE: This product meets the global product safety requirements forSELV (safety extra low voltage) rated equipment and the input voltagemust be guaranteed to remain within the SELV limits (60V maximum) inthe event of a single internal fault.Always check the integrity of the dc power supply to an INU/INUe right toits source. Never assume that the supply provided to the pick-up point ina rack is correct.Eclipse dc power, IF, tributary, auxiliary and NMS cables are not to berouted with any AC mains power lines. They are also to be kept awayfrom any AC power lines which cross them.lCarry out a complete check of the installation. When all is checked and correct,the INU is ready for power-on.oIf a PCC is installed, ensure the PCC to NCC/NPC cable is correctly fittedbefore power-on.CAUTION: Once powered up the radio frequency units will be transmitting with the pre-configured or ex-factory frequency and power settings unless the start-up transmit muteoption has been invoked. (All ODUs/RFUs shipped ex-factory have the transmit-mute setas the default unless otherwise specified).If frequency and power settings are notcorrect, interference can be caused to other links in the same geographical area.lTurn power on. For -48 Vdc connect the power cable to the NCC, and to the NPCwhere fitted. For +24 Vdc operation, connect to the PCC input.oWhere a power line filter is installed (for -48 Vdc), connect to the filter input.CAUTION: Do not turn off an INU/INUe within 10 minutes of initial turn-on, or initial turn-on after a new compact flash card is installed.CAUTION: 2W2 DC power connectors can be shorted inadvertently if applied at an angle.Always insert with correct alignment.CAUTION: Ambient temperatures must not exceed 550C (1310F). If installed in a rackcabinet, it is the ambient within the cabinet.The Eclipse INU is ready for configuration and antenna alignment.120 JULY 2018 AVIAT NETWORKS
INSTALLING THE INU AND INUE CHAPTER 6Plug-in Installation RequirementsThe table below details the plug-in requirements at installation. Unless specified by thecustomer, plug-ins will not be installed in an INU/INUe at shipment. Instead, each isindividually packed within the shipping box.For a description of the plug-ins, see the Eclipse Platform Product Description. Forconfiguring plug-ins, see Node and Terminal Plug-ins on page 1.For information on user-interface connector and cable data, refer to INU/INUe and IDUConnector and Cable Data on page 1.Table 15. Plug-in RequirementsFunction/Requirement Priority DetailsSlot AssignmentAll slots filled All slots must be filled with either a plug-in or a blanking panel.Failure to do so will compromise EMC integrity and distribution ofFAN cooling air.Universal slots1-4 on an INU1-6 on an INUeRAC, DAC, NCM, and AUX plug-ins can be fitted in any universalslot.Restricted slots7-9 on an INUeDAC, NCM, and AUX plug-ins can be fitted in any restricted slot.The exceptions are the DAC 155oM, DAC 155eM, and AUX, whichmust only be installed in slots 1 to 6 when they are to be configuredto carry/access Eclipse NMS, otherwise they can be installed inslots 7 to 9.Dedicated slots The NCC, FAN, and NPC plug-ins have dedicated slots.Protected RACs INUe Protected RACs (or ring-protected RAC with DAC 155oM) mustonly be installed in ‘above and below’ slots as indicated by the redarrows.AUX Multiple AUX plug-ins can be installed per INU/INUe.NPC Only one NPC is required to provide the NCC protection option. AnNPC must be installed in slot 4 of an INU, or slot 10 of an INUe. Ifan NPC is not installed in an INU, slot 4 is available as a universalslot.Installing / Changing Plug-insESD grounding strap Always connect yourself to the INU/INUe with an ESD groundingstrap before changing or removing a plug-in. Failure to do so cancause ESD damage to the plug-ins. Avoid hand contact with thePCB top and bottom.AVIAT NETWORKS JULY 2018 121
CHAPTER 6INSTALLING THE INU AND INUEFunction/Requirement Priority DetailsFinger-grip fasteners Plug-ins must be withdrawn and inserted using their finger-gripfasteners/pulls. Never withdraw or insert using attached cables,as damage to the plug-in connector and its PCB attachment canoccur. If not complied with, the Aviat Networks warranty may bevoided.Do not over-tighten fasteners. Hand-tighten or use only lightscrewdriver pressure.Hot-swappable Plug-ins are hot-swappable.Removal of an in-service payload plug-in will interrupt itstraffic.Removal of the NCC will affect all traffic - unless protected byan NPC.Removal / replacement of the FAN does not affect traffic.Engaging backplaneconnectorWhen installing a plug-in, ensure its backplane connector iscorrectly engaged before applying sufficient pressure to bring theplug-in panel flush with the front panel.Revision time lag When swapping or installing plug-ins, up to 60 seconds can berequired for the INU/INUe to show its revised status via the frontpanel LEDs, or via Portal.EMC integrity Plug-ins and blanking panels are held in place by captive finger-screws. Ensure the finger-screws are fastened as failure to do somay compromise EMC integrity and fan cooling.NCCsNCC Versions There are two NCC versions: V1 and V2.NCC V2 is recognized by the 4-port Ethernet NMS assembly, nofront panel fuse holder, and a 2W2C D-series power connector.NCC V1 (obsolete) has a three port Ethernet NMS assembly, afront panel fuse holder, and a small two-pin power connector.The latest software version to support NCC V1 is 5.01.44. Ifattempts are made to upgrade an INU with an NCC V1 to 6.0software, the action will not be executed; the software load willfail and the NCC will remain at the version it was originallyloaded with.Operation and inter-operation parameters for these two versionsare as follows:NCC V1 and NCC V2 can be used within the same network.NCC V1 is only suitable for the INU. It will not operate in theINUe. NCC V2 supports both INU and INUe.NCC V1 only supports the power supply redundancy capabilityof the NPC plug-in option. It does not support NPC redundancyfor backplane bus management (bus clock). NCC V2 supportsNPC redundancy for power supply and backplane busmanagement.RACs122 JULY 2018 AVIAT NETWORKS
INSTALLING THE INU AND INUE CHAPTER 6Function/Requirement Priority DetailsConnecting anddisconnecting the ODU cableat the RACNever disconnect or reconnect an ODU or IRU 600 RFU cable to aRAC without first turning the power off to the INU or withdrawingthe RAC from the backplane.NOTE: The ODU /RF U c able provides the power feed to theODU /RF U . A rc ing dur ing c onne ction a nd dis co nnec tion at theRAC on a live RAC can c ause damage to c onnec tor contactsurfaces . Power spikes c aus ed by live connec tion anddisconnec tion may al so c aus e errors on other traffic passingthro ugh the I NU /I NU e. The onl y ex c eption to l ivedisconnec tion and c onnec tion s hould be for c hecks ofprotec ted operation at link c ommis sioning.Removing RAC from apowered INUWhen removing a RAC from a powered INU, always the disengagethe RAC from the backplane before disconnecting its ODU cable.Similarly, before inserting an RAC, always reconnect the ODUcable before engaging the backplane.RAC combinations for INUe An INUe can be fitted with a maximum of six RACs for one of thefollowing combinations:Six non-protected linksOne protected/diversity link plus four non-protected linksTwo protected/diversity links plus four non-protected linksThree protected/diversity linksBefore installing more than four RACs refer to the PowerConsumption and INU Load Maximums in INU Power Supply onpage 103.)DACsDAC combinations DACs can be fitted singly or in combination to provide a mix ofinterface types and capacities provided they have a commonbackplane configuration. The backplane can be set for:- 2 Mbit/s / E1- 1.5 Mbit/s / DS1- 8 Mbit/s / E3- 3 Mbit/s / DS3- 155 Mbit/s / STM1/OC3Mux version DACs allow a mix of interfaces from a common E1 orDS1 backplane configuration.Increasing node capacity To achieve a greater node capacity, two or more INUs can beinterconnected via a DAC option.DAC 16x Mini RJ-21 tributarycable connector, or DAC16xV2/V3 HDR tributary cableconnectorEnsure correct orientation of the Mini RJ-21 connector on DAC 16xbefore pushing it home. This can be checked by the scalloped keyto one side of the connector. Additionally, a tributary cablesupplied by Aviat Networks will have the cable exiting to the rightside when viewed from the front.Ensure the connector retaining screws are not over-tightened -hand tighten or use only light screwdriver pressure.AVIAT NETWORKS JULY 2018 123
CHAPTER 6INSTALLING THE INU AND INUEFunction/Requirement Priority DetailsLine Protection (electricalDACs)Line (interface) protection is supported for paired E1/DS1, E3/DS3and STM1 electrical DACs.Line Protection (opticalDACs)Line (interface) / card protection is supported for pairedSTM1/OC3 optical DACs.Interface Protection, EthernetDAC GE3Interface / card protection is supported for paired DAC GE3 cards.NCMInstalled for E1 or DS1 loop switch operation.Two are installed for protected operation.One NCM (1+0 or 1+1) supports up to 8 E1 or DS1 tributariesdirectly on HDR connectors.One or more DAC 16xV2/V3s are additionally installed at sitesrequiring access to more than 8 tribs.Ensure the tributary connector retaining screws are not over-tightened - hand tighten or use only light screwdriver pressure.GeneralMaximum Single LinkCapacity via Eclipse NodebackplaneThe maximum drop, through plus drop, or through capacity of anEclipse Node comprising one INU/INUe is one of the following,depending on the backplane setting:200 Mbit/s / 100x E1196 Mbit/s / 127xDS14xDS3310 Mbit/s / 2xSTM1/OC3Maximum Single Link Capa-city via DPP (RAC60/60E/6X/6XE DPP con-nected to DAC GE or DACGE3)366 Mbps for Ethernet traffic or mixed-mode Ethernet withTDM, using a 256 QAM maximum throughput modulationprofile. This is the link (air) capacity. If all traffic is Ethernet,the nominal L2 throughput maximum is 365 Mbps (1518byte frames); the nominal L1 throughput maximum is 465Mbps (64 byte frames).Antistatic bags Enclose spare plug-ins, or plug-ins to be returned for service, inan antistatic bag. When handling a plug-in to or from an antistaticbag, do so at the INU/INUe and only when you are connected to theINU/INUe via an ESD ground strap.Spare blank panels Keep any removed blanking panels for future use.124 JULY 2018 AVIAT NETWORKS
USER MANUALAppendix A. Antennas certified for usewith IRU 600v4 at 5.8GHzThe following table lists all the antennas certified for use with IRU 600v4 at 5.8GHz.Manufacturer Part Number Antenna Gain(dBi)Antenna Size ft(meters) Antenna TypeRFS MA0528-19AN 19 0.5 Flat panelRFS MA0528-23AN 23 1 Flat panelRFS MA0528-28AN 28 2 Flat panelRFS SPF2-52CN1S 28.5 2 (0.6) ParabolicRFS SPF3-52CN1S 32 3 (0.9) ParabolicRFS SPF4-52CN1S 34.4 4 (1.2) ParabolicRFS SPF6-52CN1S 38.1 6 (1.8) ParabolicRFS SDF3-52CN1S1 32 3 (0.9) ParabolicRFS SDF4-52CN1S1 34.4 4 (1.2) ParabolicRFS SDF6-52CN1S1 38.1 6 (1.8) ParabolicRFS UXA6-U57AC 39 6 (1.8) ParabolicRFS UXA8-U57AC 41.6 8 (2.4) ParabolicRFS PADX6-U57AC1S1R 38.9 6 (1.8) ParabolicRFS PADX8-U57AC1S1R 41.4 8 (2.4) ParabolicRFS PAD6-59BC1S1R 38 6 (1.8) ParabolicRFS PAD8-59AC1S1R 40.7 8 (2.4) ParabolicRFS SU6-59By 38.1 6 (1.8) ParabolicRFS SU4-59By 34.7 4 (1.2) ParabolicRFS DA6-59BC 38.4 6 (1.8) ParabolicRFS DA8-59Ay 40.9 8 (2.4) ParabolicRFS UA8-59Ay 40.9 8 (2.4) ParabolicRFS SUX6-59By 37.8 6 (1.8) ParabolicRFS SUX4-59Ay 33.8 4 (1.2) ParabolicRFS DAX4-59AC 33.8 4 (1.2) ParabolicRFS DAX6-59BC 38 6 (1.8) ParabolicRFS DAX8-59Ay 40.7 8 (2.4) ParabolicRFS UXA4-59Ay 33.8 4 (1.2) ParabolicRFS UXA6-59Cy 38 6 (1.8) Parabolic260-668066-001 JULY 2018 125
APPENDIX A, ANTENNAS CERTIFIED FOR USE WITH IRU 600V4 AT 5.8GHZManufacturer Part Number Antenna Gain(dBi)Antenna Size ft(meters) Antenna TypeRFS UXA8-59By 40.6 8 (2.4) ParabolicRFS PADX6-W59BC1S1R 37.9 6 (1.8) ParabolicRFS PADX8-W59AC1S1R 40.4 8 (2.4) ParabolicRFS UXA6-W59BC 38.1 6 (1.8) ParabolicRFS UXA8-W59AC 40.6 8 (2.4) ParabolicRFS SC3-W60y 31.5 3 (0.9) ParabolicRFS SB4-W60y 34.3 4 (1.2) ParabolicRFS SB6-W60y 38.2 6 (1.8) ParabolicRFS SCX3-W60y 31.5 3 (0.9) ParabolicRFS SBX4-W60y 34.3 4 (1.2) ParabolicRFS SBX6-W60y 38.2 6 (1.8) ParabolicRFS PA4-W57BC1S1 35.5 4 (1.2) ParabolicRFS PA6-W57BC1S1 39 6 (1.8) ParabolicRFS PA8-W57AC1S1 41.5 8 (2.4) ParabolicRFS PAD6-W57BC1S1R 38.9 6 (1.8) ParabolicRFS PAD8-W57AC1S1R 41.4 8 (2.4) ParabolicRFS PADX6-W57AC1S1R 38.7 6 (1.8) ParabolicRFS PADX8-W57AC1S1R 41.2 8 (2.4) ParabolicRFS DA6-W57BC 39 6 (1.8) ParabolicRFS DA6-W57BC 41.5 8 (2.4) ParabolicRFS UXA6-W57AC 38.9 6 (1.8) ParabolicRFS UXA8-W57AC 41.4 8 (2.4) ParabolicCommScope P4F-52/A 34.9 4 ParabolicCommScope P6F-52/A 37.6 6 ParabolicCommScope PX4F-52/A 34.9 4 ParabolicCommScope PX6F-52/A 37.6 6 ParabolicCommScope P4F-57W/A 35 4 ParabolicCommScope P6F-57W/A 38.5 6 ParabolicCommScope P8F-57W 41.2 8 ParabolicCommScope P10F-57W 42.9 10 ParabolicCommScope P4-57W/A 35 4 ParabolicCommScope PL6-57W/A 38.5 6 ParabolicCommScope PL8-57W 41.2 8 ParabolicCommScope PL10-57W 42.9 10 ParabolicCommScope HP4F-57W/A 35 4 Parabolic126 AVIAT NETWORKS
USER MANUALManufacturer Part Number Antenna Gain(dBi)Antenna Size ft(meters) Antenna TypeCommScope HP6F-57W/A 38.5 6 ParabolicCommScope HP8F-57W 41.2 8 ParabolicCommScope HP10F-57W 42.9 10 ParabolicCommScope HP4-57W/A 35 4 ParabolicCommScope HP6-57W/A 38.5 6 ParabolicCommScope HP8-57W 41.2 8 ParabolicCommScope HP10-57W 42.9 10 ParabolicCommScope PAR8-59 40.2 8 ParabolicCommScope PARX8-59 40.2 8 ParabolicCommScope HX6-6W 39.1 6 ParabolicCommScope USX6-6W 38.4 6 ParabolicCommScope HP6-59 37.9 6 ParabolicCommScope HP8-59 40.8 8 ParabolicCommScope HP10-59 42.3 10 ParabolicCommScope HP12-59 44.4 12 ParabolicCommScope PARX8-59 40.1 8 ParabolicCommScope PARX10-59 42.4 10 ParabolicCommScope UHX6-59 38.1 6 ParabolicCommScope UHX8-59 40.6 8 ParabolicCommScope UHX10-59 42.6 10 ParabolicCommScope UHX12-59 44.1 12 ParabolicCommScope HPX4-59 34.1 4 ParabolicCommScope HPX6-59 38.1 6 ParabolicCommScope HPX8-59 40.6 8 ParabolicCommScope HPX10-59 42.4 10 ParabolicCommScope PAR8-59 40.1 8 ParabolicCommScope PAR10-59 42.7 10 Parabolic260-668066-001 JULY 2018 127
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