Presentation 2001/2/16
JetGun Sat"TOPPU"
Kyoichi Ui, Ryuichi Hodoshima, Naohide Maeda, Hideto Okada, Naoki Miyashita, Masafumi Iai, Osamu Mori, Saburo Matunaga,
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Abstract(in English) In recent years, the research of the formation flight has become more attractive and important. It is expected that the formation flight technology is applied to the multi-point observation, maintenance, inspection, recovery of an uncontrolled satellite. But we have many subjects that should be solved to realize this technology. Under this situation, we propose the micro satellite for the verification of the formation flight technologies. This satellite is the mothership-daughtership satellite equipped the docking mechanism, tether reel mechanism, gas jet gun. In this paper we explain about the conceptual design result and propose the on-orbit experiments. Moreover we will report the curent status on this satellite development.
Keyword(in Japanese) (See Japanese page)
Keyword(in English) Small mothership-daughtership satellite / Docking mechanism / Tether reel mechanism / Gasjet gun / Non-contact recharging system / Ground station network
Paper # SANE2000-176,SAT2000-125
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Committee SAT
Conference Date 2001/2/16(1days)
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Registration To Satellite Telecommunications (SAT)
Language JPN
Title (in Japanese) (See Japanese page)
Sub Title (in Japanese) (See Japanese page)
Title (in English) JetGun Sat"TOPPU"
Sub Title (in English)
Keyword(1) Small mothership-daughtership satellite
Keyword(2) Docking mechanism
Keyword(3) Tether reel mechanism
Keyword(4) Gasjet gun
Keyword(5) Non-contact recharging system
Keyword(6) Ground station network
1st Author's Name Kyoichi Ui
1st Author's Affiliation Department of Mechanical and Aerospace Engineering, Graduate school of Science and Engineering, Tokyo Institute of Technology()
2nd Author's Name Ryuichi Hodoshima
2nd Author's Affiliation Department of Mechanical and Aerospace Engineering, Graduate school of Science and Engineering, Tokyo Institute of Technology
3rd Author's Name Naohide Maeda
3rd Author's Affiliation Department of Mechanical and Aerospace Engineering, Graduate school of Science and Engineering, Tokyo Institute of Technology
4th Author's Name Hideto Okada
4th Author's Affiliation Department of Mechanical and Aerospace Engineering, Graduate school of Science and Engineering, Tokyo Institute of Technology
5th Author's Name Naoki Miyashita
5th Author's Affiliation Department of Mechanical and Aerospace Engineering, Graduate school of Science and Engineering, Tokyo Institute of Technology
6th Author's Name Masafumi Iai
6th Author's Affiliation Department of Mechanical and Aerospace Engineering, Graduate school of Science and Engineering, Tokyo Institute of Technology
7th Author's Name Osamu Mori
7th Author's Affiliation Department of Mechanical and Aerospace Engineering, Graduate school of Science and Engineering, Tokyo Institute of Technology
8th Author's Name Saburo Matunaga
8th Author's Affiliation Department of Mechanical and Aerospace Engineering, Graduate school of Science and Engineering, Tokyo Institute of Technology
Date 2001/2/16
Paper # SANE2000-176,SAT2000-125
Volume (vol) vol.100
Number (no) 638
Page pp.pp.-
#Pages 7
Date of Issue