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http://dx.doi.org/10.5140/JASS.2003.20.4.383

ELECTROMAGNETIC COMPATIBILITY DESIGN FOR KOMPSAT-2  

Lee, Na-Young (Korea Aerospace Research Institute)
Lee, Jin-Ho (Korea Aerospace Research Institute)
Publication Information
Journal of Astronomy and Space Sciences / v.20, no.4, 2003 , pp. 383-392 More about this Journal
Abstract
It is quite essential that requirements allocation and analysis would be done for the electromagnetic compatibility (EMC) of all units when designing a satellite. Although KOMPSAT-2 inherits relatively large portions of the electrical designs from KOMPSAT-1, it has a new instrument and different combinations of sensors and actuators as well as their driving circuitry. Many requirements for the electromagnetic compatibility were modified and newly allocated for KOMPSAT-2. Naturally, they must be justified through analyses from the early stage of the program. In this paper, the EMC compatibility requirements for KOMPSAT2 are presented and verified for their suitability. In addition, some results, which were obtained from various analyses, are presented and discussed.
Keywords
KOMPSAT-2; electro-magnetic compatibility; conducted emission; conducted susceptibility; radiated emission; radiated susceptibility; spacecraft;
Citations & Related Records
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  • Reference
1 /
[ KARI ] / KOMPSAT-2 Power Transient Analysis Report, K2-KS-RP-0114
2 /
[ ELOP ] / MSC CDR Data Package
3 Requirements for the Units EMC Design /
[ KARI ] / Perfromance and Tests, K2-SP-410-005
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[ DOD ] / MIL-STD-461E
5 /
[ KARI ] / KOMPSAT2 EDI CDA data package
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[ KARI ] / K2-NT-0127-T-ASTR
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[ KARI ] / K2-SP-330-003