Electrical System Design of Prototype Communication Satellite
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概要
- 論文の詳細を見る
The major goal of this study is to design a model of the domestic communication satellite namely by 2005SAT. The key features of 2005SAT bus system have 3-axis stabilized platform for transfer orbit and on-orbit operations, main bus voltage with 42.5V and dual mode propulsion system. And also, the electrical subsystem of 2005SAT is designed to meet the performance requirements specified in bus system and subsystem specification during all expected spacecraft operations. The electerical bus system is designed to accommodate the communication payload requirements including the fifteen transponders and a 10 years design life. The basic design of electronic units and electrical interface of AOCS, EPS and TC&R subsystems for an ETB configulation is performed through the analysis and trade-off study of each subsystem.
- 2001-10-16
著者
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Choi Sung-bong
Communication Satellite Systems Department Kari
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Kim Z‐c
Korea Aerospace Res. Inst. Daejeon Kor
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Choi J‐d
Korea Aerospace Res. Inst. Daejon Kor
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Choi S‐b
Coms Program Office Korea Aerospace Research Institute
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Choi Seong-bong
Korea Aerospace Researcg Institute
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Kim Zeen-Chul
Korea Aerospace Research Institute
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Choi Jae-Dong
Korea Aerospace Researcg Institute
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Park Young-Woong
Korea Aerospace Researcg Institute
関連論文
- Reliable and Compute Effective Onboard Stationkeeping System for Geostationary Satellites
- Reliable and Compute Effective Onboard Stationkeeping System for Geostationary Satellites(System Engineerint-III)
- Electrical System Design of Prototype Communication Satellite
- Conceptual Design of Communication, Ocean and Meteorological Satellite System
- Conceptual Design of Communication, Ocean and Meteorological Satellite System(System Engineering-II)
- A BUS System Conceptual Design of Experimental Communication Satellite
- KARI's Testing Facilities and Technologies for GEO Satellite Development (2002 Joint Conference on Satellite Communications(JC-SAT2002)--衛星通信技術及び一般)