DocumentCode :
2662137
Title :
A Study for payload interface design of GEO satellite
Author :
Choi, Jae-Dong ; Park, Jong-seok ; Yang, Koon-ho
Author_Institution :
Korea Aerosp. Res. Inst., Daejeon, South Korea
fYear :
2009
fDate :
18-22 Oct. 2009
Firstpage :
1
Lastpage :
5
Abstract :
Mechanical, thermal and electrical interface design is used to integrate payloads on the GEO satellite. This paper defines the mechanical, thermal and electrical interface specification and the detailed design result of payload installed to perform the communication and ocean monitoring mission of the GEO Satellite. For mechanical and thermal interface, the payload equipments are designed to avoid mutual interference and temperature limit condition between the units. The electric interface for Command, Telemetry and Low Speed Serial Bus design with satellite platform is analyzed.
Keywords :
artificial satellites; GEO satellite; electrical interface design; mechanical interface design; payload interface design; thermal interface design; Artificial satellites; Filters; Interference; Meteorology; Ocean temperature; Payloads; Reflector antennas; Satellite broadcasting; Thermal conductivity; Underwater communication;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Telecommunications Energy Conference, 2009. INTELEC 2009. 31st International
Conference_Location :
Incheon
Print_ISBN :
978-1-4244-2490-0
Electronic_ISBN :
978-1-4244-2491-7
Type :
conf
DOI :
10.1109/INTLEC.2009.5352079
Filename :
5352079
Link To Document :
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