Abstract
This document contains a process to establish performance requirements for the purpose of ensuring space systems electromagnetic compatibility (EMC). The engineering issues to be addressed in order to achieve system-level EMC are identified herein, with guidance and rationale towards achieving specification conformance. The method for the derivation of typical equipment-level requirements from a space-system-level requirement is illustrated. This document also aids in the selection of tailored requirements for a specific mission (see Annex A).
General information
-
Status: PublishedPublication date: 2022-06Stage: International Standard published [60.60]
-
Edition: 2Number of pages: 46
-
Technical Committee :ISO/TC 20/SC 14
- RSS updates
Life cycle
-
Previously
WithdrawnISO 14302:2002
-
Now