Attachment System description

This document pretains to SES-LIC-INTR2019-03638 for License on a Satellite Earth Station filing.

IBFS_SESLICINTR201903638_1938323

SAILOR600/900 Viasat Ka pTRIA CE approval fundamentals Document number: 99-164707-A Date: 30 January 2019 Author: Jesper M. Andersen Printed version of this document is only valid if lifecycle is indicated as released in the top banner Copyright© Thrane & Thrane A/S trading as Cobham SATCOM Lundtoftegaardsvej 93D, DK-2800 Kgs. Lyngby, Denmark ALL RIGHTS RESERVED Filename: 99-164707-A_SAILOR900-Viasat_vs-CE-compliance.docx

SAILOR600/900 Viasat Ka pTRIA 99-164707-A CE approval fundamentals REVISION HISTORY Rev. Date App. Section Description / Remarks A 23-11-2018 CMP All Original  Thrane & Thrane A/S trading as Cobham SATCOM This Document and any other appended documents and drawings are of  copyright to Thrane & Thrane A/S. It contains proprietary information which is disclosed for information purposes only. The contents of this document shall not in whole or in part be used for any other purpose; be disclosed to any member of the recipients organisation not having a need to know such information or to any third party, individual, organisation or Government; be stored in any retrieval system or be produced or transmitted in any form by photocopying or any optical, mechanical or other means without prior permission of Thrane & Thrane A/S. 30 January 2019 Page i of ii

SAILOR600/900 Viasat Ka pTRIA 99-164707-A CE approval fundamentals Table of Contents Table of Contents ................................................................................................................... ii List of Schematics .................................................................................................................. ii 1. Scope and Purpose........................................................................................................ 1 1.1. Related Documents .................................................................................................. 1 1.1.1. Standards............................................................................................................ 1 1.1.2. Test reports associated to this evaluation............................................................ 1 1.2. References ............................................................................................................... 1 1.3. Abbreviations ............................................................................................................ 1 2. Introduction .................................................................................................................... 2 3. SAILOR 600/900 Viasat Ka evaluation ........................................................................... 3 3.1. Required evaluations ................................................................................................ 3 3.2. Schematics ............................................................................................................... 4 3.2.1. PIM, hot-swap ..................................................................................................... 4 3.2.2. PIU and SPOCK module ..................................................................................... 5 4. Required standards for compliance to CE and FCC ....................................................... 6 List of Schematics Schematic 1 ........................................................................................................................... 4 Schematic 2 ........................................................................................................................... 5 30 January 2019 Page ii of ii

SAILOR600/900 Viasat Ka pTRIA 99-164707-A CE approval fundamentals 1. Scope and Purpose This document will describe the thoughts behind the CE conformity and approval of the SAILOR 600 Viasat Ka (part number 407060D) and 900 Viasat Ka (part number 407090F) VSAT antenna system. The purpose of this document is to keep the thoughts behind the CE-conformity and the approval process of the 407060D and 407090F in one document, as the complete evidence consists of several reports from several CE evaluations of different products. 1.1. Related Documents 1.1.1. Standards DS EN 60950-1-2006 IEC 60695-2-11 EN 62368-1:2014 EN 301489-1, EN 301489-12 EN 301843-1, EN 301843-6 EN 60945:2004 1.1.2. Test reports associated to this evaluation 99-163859-B or newer (overview document) 99—153805-A (safety evaluation of SAILOR 900 VSAT HP) 99-158477-A (EN/IEC60950-22) 99-161900-A (IP evaluation) 99-153806-A (EN/IEC60950-1 evaluation of the “APS” AC/DC SMPS) 99-152389-A (EN 60945 evaluation of SAILOR 100GX) 1.2. References [1] 98-164678-A: Reference manual. [2] 99-164903-A: CE-approval test-instructions: 1.3. Abbreviations ACU Antenna Control Unit ADU Above Deck Unit (antenna) BDU Below Deck Unit CE European Community (EU) marking GMU GX Modem Unit PIM mpTRIA Interface Module PIU mpTRIA Interface Unit PWB Printed Wiring Board (aka PCB, Printed Circuit Board) TBD To Be Defined TBC To Be Confirmed VIM VSAT Interface Module 30 January 2019 Page 1 of 6

SAILOR600/900 Viasat Ka pTRIA 99-164707-A CE approval fundamentals 2. Introduction This document will describe the thoughts behind the CE conformity and approval of the SAILOR 600 Viasat Ka (part number 407060D), and SAILOR 900 Viasat Ka(part number 407090F) VSAT antenna systems. . 30 January 2019 Page 2 of 6

SAILOR600/900 Viasat Ka pTRIA 99-164707-A CE approval fundamentals 3. SAILOR 600/900 Viasat Ka evaluation pTRIA product differs from the other SAILOR VSAT models, primarily by the PIM (pTRIA Interface Module) vs the VIM (VSAT Interface Module) and the addition of the PIU (pTRIA Interface Unit) between the ACU and any different ADUs. Based on the above, following interpretation and assumptions are create (in relation to Low Voltage Directive, LVD, and Radio Equipment Directory, RED, with respect to standards EN/IEC 60950-1, EN/IEC 60950-22 or EN/IEC 62368-1:2014): VIM has identical circuitry with VIM, which was evaluated in the SAILOR 900 HP evaluation and SAILOR 600Ku. PIU is deem compliant to the above mention EU directives and standards, based on the fact, that the electrical behaviour between ACU and VIM (located in the ADU as first entry point from the ACU). Furthermore is the circuitry in the PIU very simple, consisting of an input connector (N-type connector), and solid cupper trace on the PWB, and an output connector (N-type connector). The enclosure of the PIU is identical to the GMU, besides some minor changes to the back panel. Due to this, the applicable IP rating is similar to the GMU, IP class 3X verified by EN/IEC 60950-1 clause 4.6. 3.1. Required evaluations To show compliance for LVD and RED, the ACU was originally evaluated, as described in document: 99-153805-A, while the AC/DC converter in the ACU was evaluated as described in 99-153806-A, in accordance to EN/IEC 60950-1. Furthermore, was the ACU evaluated in accordance with EN/IEC 62368-1 as described in 99- 153851-B. For evidence of further compliance to RED (in terms for EMC and RF matters), Viasat provides the required reports of the evaluation of the pTRIA and SPOCK modules. Cobham SATCOM submit evaluations of the two complete systems in terms of EMC. Test is conduct by CTC advanced, Saarbrücken in Germany. 30 January 2019 Page 3 of 6

SAILOR600/900 Viasat Ka pTRIA 99-164707-A CE approval fundamentals 3.2. Schematics As described in Schematic 2, the N-connector in the PIM, supplying the ADU, saying that the full current for the ADU flows through the N-connector and its associated circuitry. As noted below in 3.2.1, the circuit (the PIM hot-swap) defines the limit of the current available in the rest of the modules in the ADU, and hence any further testing is not required, as previous product evaluations includes the required tests. 3.2.1. PIM, hot-swap The PIM hot-swap circuitry, in which the highest current available is present through Q4600. This circuitry is close to 100% identical with the VIM. Schematic 1 The only major difference is the current limit, which is reduced to 3 Adc in PIM. 30 January 2019 Page 4 of 6

SAILOR600/900 Viasat Ka pTRIA 99-164707-A CE approval fundamentals 3.2.2. PIU and SPOCK module The PIU is connected between the ACU and the ADU, to enable the communication to the mpTRIA in the ADU. The connections on a higher level is illustrate in below block diagram. Block diagram Schematic 2 30 January 2019 Page 5 of 6

SAILOR600/900 Viasat Ka pTRIA 99-164707-A CE approval fundamentals 4. Required standards for compliance to CE and FCC Below table lists all applicable standards, and if already evaluated the associated product number: Standard Show compliance for Responsible Document number / explanation SAILOR 600 SAILOR 900 EN/IEC 60950-1 LVD Safety Cobham 99-153806-A, + 99-153805-A X X EN/IEC 60950-22 LVD Safety - outdoor equipment Cobham 99-158477-A + 99-161900-A - X EN/IEC 60950-22 LVD Safety – outdoor equipment Cobham 99-148528-A X - EN/IEC 62368-1 LVD Safety (the “new standard) Cobham 99-153851-B X X (ACU only) EN/IEC 60945 Maritime safety Cobham 99-152389-A, 99-143334-A X X EN/IEC 60945 Maritime safety Cobham 99-149122-A X - EN 301489-1 EMC, radio equipment Cobham/Viasat Viasat: report for pTRIA. Cobham: report for the system X X EN 301489-12 EMC, VSAT Cobham/Viasat Viasat: report for pTRIA. Cobham: report for the system X X EN 301843-1 EMC, maritime radio equipment Cobham Cobham provide report from CTC X X EN 301843-6 EMC, maritime VSAT Cobham Cobham provide report from CTC X X EN 55032 EMC conducted Cobham Cobham provide report from CTC X X FCC part 15 EMC, North America Cobham/Viasat Viasat: report for pTRIA. Cobham: report for the system X X EN 303978 RF spectrum Viasat Viasat provides report for the pTRIA BUC X X Fcc part 25 RF spectrum, North America/Canada Viasat Viasat provides report for the pTRIA BUC X X EN 62311 Health vs radiation Cobham/Viasat X X Cobham delivers figures and simulations for both platforms to FCC part 1 Health vs radiation, North America Cobham/Viasat X X Viasat, prior to RF-spectrum reports. IC RSS 102 Health vs radiation, Canada Cobham/Viasat X X 30 January 2019 Page 6 of 6


Document Created: 2019-01-30 13:37:59
Document Modified: 2019-01-30 13:37:59
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