BS ISO 14302:2002
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
Aerospace series. Space systems. Electromagnetic compatibility requirements
Hardcopy , PDF
03-08-2022
English
14-04-2003
Committee |
ACE/68
|
DevelopmentNote |
Supersedes 99/716810 DC (04/2003)
|
DocumentType |
Standard
|
Pages |
58
|
PublisherName |
British Standards Institution
|
Status |
Superseded
|
SupersededBy | |
Supersedes |
This International Standard establishes 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.
Standards | Relationship |
ISO 14302:2002 | Identical |
NASA HDBK 4002 : 2011 | MITIGATING IN-SPACE CHARGING EFFECTS - A GUIDELINE |
SAE ARP1972A | Recommended Measurement Practices and Procedures for EMC Testing |
CISPR 22:2008 | Information technology equipment - Radio disturbance characteristics - Limits and methods of measurement |
SAE ARP1870A | Aerospace Systems Electrical Bonding and Grounding for Electromagnetic Compatibility and Safety |
MIL-STD-461 Revision G:2015 | REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT |
IEC 61000-4-2:2008 | Electromagnetic compatibility (EMC) - Part 4-2: Testing and measurement techniques - Electrostatic discharge immunity test |
ISO 7137:1995 | Aircraft — Environmental conditions and test procedures for airborne equipment |
SAE ARP5412B | Aircraft Lightning Environment and Related Test Waveforms |
CISPR 16-1:1999+AMD1:2002 CSV | Specification for radio disturbance and immunity measuring apparatus and methods - Part 1: Radio disturbance and immunity measuring apparatus |
NASA HDBK 4001 : 0 | ELECTRICAL GROUNDING ARCHITECTURE FOR UNMANNED SPACECRAFT |
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