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.
BS EN 16603-20-07 on electromagnetic compatibility for space system is relevant to:
Electromagnetic compatibility (EMC) of a space system or equipment is the ability to function satisfactorily in its electromagnetic environment without introducing intolerable electromagnetic disturbances to anything in that environment.
The space system is designed to be compatible with its external natural, induced, or man-made electromagnetic environment.
BS EN 16603-20-07 provides you with the system requirements, verification plan, and testing methods for the space equipment that you manufacture. BS EN 16603-20-07 guidelines enable you to comply with electromagnetic emission range requirements. BS EN 16603-20-07 ensures the smooth operation and safety of your appliances, increasing their lifespan.
EN 16603-20-07:2014