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SRPS EN 16603-20-07:2016

Space engineering - Electromagnetic compatibility

Sep 21, 2016
95.99   Withdrawal of Standard   Oct 31, 2022

General information

95.99     Oct 31, 2022

ISS

S020

European Norm

49.140  

English  

Van plana 2016

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Scope

EMC policy and general system requirements are specified in ECSS-E-ST-20.
This ECSS-E-ST-20-07 Standard addresses detailed system requirements (Clause 4), general test conditions, verification requirements at system level, and test methods at subsystem and equipment level (Clause 5) as well as informative limits (Annex A).
Associated to this standard is ECSS-E-ST-20-06 “Spacecraft charging”, which addresses charging control and risks arising from environmental and vehicle-induced spacecraft charging when ECSS-E-ST-20-07 addresses electromagnetic effects of electrostatic discharges.
Annexes A to C of ECSS-E-ST-20 document EMC activities related to ECSS E ST 20 07: the EMC Control Plan (Annex A) defines the approach, methods, procedures, resources, and organization, the Electromagnetic Effects Verification Plan (Annex B) defines and specifies the verification processes, analyses and tests, and the Electromagnetic Effects Verification Report (Annex C) document verification results. The EMEVP and the EMEVR are the vehicles for tailoring this standard.
This standard may be tailored for the specific characteristic and constrains of a space project in conformance with ECSS-S-ST-00.

Life cycle

NOW

WITHDRAWN
SRPS EN 16603-20-07:2016
95.99 Withdrawal of Standard
Oct 31, 2022

REVISED BY

PUBLISHED
SRPS EN 16603-20-07:2022

Related project

Adopted from EN 16603-20-07:2014