Space engineering. Electromagnetic compatibility
Space engineering. Electromagnetic compatibility
What is BS EN 16603-20-07 - Electromagnetic compatibility for space system about? EMC policy and general system requirements are specified in ECSS-E-ST-20. BS EN 16603-20-07 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 BS EN 16603-20-07 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. Who is BS EN 16603-20-07 - Electromagnetic compatibility for space system for? BS EN 16603-20-07 on electromagnetic compatibility for space system is relevant to:
Space equipment manufacturers Design engineers Aerospace and defence industries Quality compliance personnel
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