Presentation | 2006-11-24 Lessons Learned of Small Satellite REIMEI and Next Standard Bus of Small 3 Axis Satellite Hirobumi Saito, Masato Nakamura, Keisuke Yoshihara, Seisuke Fukuda, |
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Abstract(in Japanese) | (See Japanese page) |
Abstract(in English) | Japan Aerospace Exploration Agency has a plan to develop small satellite standard bus for various scientific mission and disaster monitoring missions. The satellite bus is a class of 200-400Kg mass with three-axis control capability of 0.02°accuracy. This paper describes the characteristics of the small satellite standard bus, comparing with overseas examples. |
Keyword(in Japanese) | (See Japanese page) |
Keyword(in English) | Small Satellite / Satellite Bus / Space Science |
Paper # | SANE2006-109 |
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Conference Information | |
Committee | SANE |
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Conference Date | 2006/11/17(1days) |
Place (in Japanese) | (See Japanese page) |
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Topics (in Japanese) | (See Japanese page) |
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Paper Information | |
Registration To | Space, Aeronautical and Navigational Electronics (SANE) |
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Language | JPN |
Title (in Japanese) | (See Japanese page) |
Sub Title (in Japanese) | (See Japanese page) |
Title (in English) | Lessons Learned of Small Satellite REIMEI and Next Standard Bus of Small 3 Axis Satellite |
Sub Title (in English) | |
Keyword(1) | Small Satellite |
Keyword(2) | Satellite Bus |
Keyword(3) | Space Science |
1st Author's Name | Hirobumi Saito |
1st Author's Affiliation | Japan Aerospace Exploration Agency() |
2nd Author's Name | Masato Nakamura |
2nd Author's Affiliation | Japan Aerospace Exploration Agency |
3rd Author's Name | Keisuke Yoshihara |
3rd Author's Affiliation | Japan Aerospace Exploration Agency |
4th Author's Name | Seisuke Fukuda |
4th Author's Affiliation | Japan Aerospace Exploration Agency |
Date | 2006-11-24 |
Paper # | SANE2006-109 |
Volume (vol) | vol.106 |
Number (no) | 380 |
Page | pp.pp.- |
#Pages | 6 |
Date of Issue |