Presentation 2000/11/30
A BUS System Conceptual Design of Experimental Communication Satellite
Zeen-Chul Kim, Seong-Bong Choi, Mun-Kyung Nam, Koon-Ho Yang, Jae-Dong Choi,
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Abstract(in English) The 2005SAT is designed to fit within the standard fairings for all compatible launch vehicles including Ariane IV, V and Atlas II/III. The 2005SAT configuration is compatible with single launch, upper or lower position of dual launch. Two offset-fed Gregorian antennae are located on the earth panel of the 2005SAT for Ku-band and Ka-band communication services. The 2005AST bus is 3-axis stablized platform both for transfer orbit and on-orbit operations. The attitude control logic is used quaternion using gyro data and have the compensation logic for gyrobias update by the ESA and the SSA data. The 2005SAT Electrical Power Subsystem (EPS) is designed a regulated directed-energy transfor configuration that minimize the losses between the solar array and loads while minimizing the complexity and mass of load power converters. The duel-mode propulsion scheme is selected for 2005SAT. TC&R subsystem is conceptually designed to determine specifications of processor speed, RAM and ROM size, command-telemetry format and data bus type.
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Paper # SAT2000-81
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Conference Information
Committee SAT
Conference Date 2000/11/30(1days)
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Registration To Satellite Telecommunications (SAT)
Language ENG
Title (in Japanese) (See Japanese page)
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Title (in English) A BUS System Conceptual Design of Experimental Communication Satellite
Sub Title (in English)
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1st Author's Name Zeen-Chul Kim
1st Author's Affiliation Korea Aerospace Research Institute()
2nd Author's Name Seong-Bong Choi
2nd Author's Affiliation Korea Aerospace Research Institute
3rd Author's Name Mun-Kyung Nam
3rd Author's Affiliation Korea Aerospace Research Institute
4th Author's Name Koon-Ho Yang
4th Author's Affiliation Korea Aerospace Research Institute
5th Author's Name Jae-Dong Choi
5th Author's Affiliation Korea Aerospace Research Institute
Date 2000/11/30
Paper # SAT2000-81
Volume (vol) vol.100
Number (no) 483
Page pp.pp.-
#Pages 7
Date of Issue