Presentation | 2000/6/23 SANE2000-34 Method of designing for 500kg class satellite Shigeru Usuki, |
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PDF Download Page | PDF download Page Link |
Abstract(in Japanese) | (See Japanese page) |
Abstract(in English) | The method of designing for 500kg class satellite is described in the case of the Mission Demonstration test Satellite-1(MDS-1). MDS-1 is classed as small or middle satellite in NASDA. The purposes of MDS-1 are to verify the space demonstration of commercial parts and components, and to evaluate the method of short term and low cost development. |
Keyword(in Japanese) | (See Japanese page) |
Keyword(in English) | Mission Demonstration test Satellite / MDS-1 / commercial parts / short term and low cost development |
Paper # | SANE2000-34 |
Date of Issue |
Conference Information | |
Committee | SANE |
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Conference Date | 2000/6/23(1days) |
Place (in Japanese) | (See Japanese page) |
Place (in English) | |
Topics (in Japanese) | (See Japanese page) |
Topics (in English) | |
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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) | SANE2000-34 Method of designing for 500kg class satellite |
Sub Title (in English) | |
Keyword(1) | Mission Demonstration test Satellite |
Keyword(2) | MDS-1 |
Keyword(3) | commercial parts |
Keyword(4) | short term and low cost development |
1st Author's Name | Shigeru Usuki |
1st Author's Affiliation | National Space Development Agency of Japan() |
Date | 2000/6/23 |
Paper # | SANE2000-34 |
Volume (vol) | vol.100 |
Number (no) | 162 |
Page | pp.pp.- |
#Pages | 8 |
Date of Issue |