Title :
Electrical interfaces compatibility analysis for the COMS EPS
Author :
Koo, Ja-Chun ; Kim, Eui-Chan
Author_Institution :
Korea Aerosp. Res. Inst., Daejeon
Abstract :
The COMS (communication, ocean and meteorological satellite) EPS (electrical power subsystem) is derived from an enhanced Eurostar 3000. The COMS EPS can offer a bus power capability of 3 kW. The aim of this analysis is to verify the electrical compatibility of the interfaces which exist between COMS EPS equipments and external equipments. For each interface, this study checked the compatibility between equipments for the power links, commands, digital telemetry, analog telemetry and failure condition. In addition with this interface compatibility verification, this study outputs electrical and manufacturing constraints to be applied at harness level.
Keywords :
artificial satellites; meteorological instruments; satellite communication; space vehicle power plants; telemetry; COMS EPS; Eurostar 3000; analog telemetry; communication, ocean and meteorological satellite; digital telemetry; electrical interfaces compatibility; electrical power subsystem; failure condition; power links; Aerospace electronics; Batteries; Frequency; Fuses; Manufacturing; Performance analysis; Power electronics; Telemetry; Voltage; Wires;
Conference_Titel :
Power Electronics, 2007. ICPE '07. 7th Internatonal Conference on
Conference_Location :
Daegu
Print_ISBN :
978-1-4244-1871-8
Electronic_ISBN :
978-1-4244-1872-5
DOI :
10.1109/ICPE.2007.4692402
