| Presentation | 2007-11-30 Development of Control System for Microgravity Experimental System that Uses High Altitude Balloon : Experimental Report and Examination of Pullout Control for Supersonic Flight Shouhei KADOOKA, Shujiro SAWAI, Shin-ichiro SAKAI, Nobutaka BANDO, Takehiko ISHIKAWA, Tatsuaki HASHIMOTO, |
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| PDF Download Page |  PDF download Page Link |
| Abstract(in Japanese) | (See Japanese page) |
| Abstract(in English) | The microgravity experimental system that uses the high altitude balloon is now developed in ISAS/JAXA. This experimental method is, 1) Experiment body is raised to 40km altitude by the high altitude balloon, 2) The experimental system is separated, 3) A free fall for 30-40 seconds is achieved. In the experiment, the experiment body enters a supersonic state when the free fall time exceeds about 30 seconds. Therefore, it can be expected that the body offers a supersonic flight environment besides the microgravity experiment. In this paper, explanation of microgravity experiment was shown, and supersonic flight by mounting engine was considered. |
| Keyword(in Japanese) | (See Japanese page) |
| Keyword(in English) | Microgravity / Pullout Control / Supersonic Flight / Balloon |
| Paper # | SANE2007-82 |
| Date of Issue |
| Conference Information | |
| Committee | SANE |
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| Conference Date | 2007/11/23(1days) |
| Place (in Japanese) | (See Japanese page) |
| Place (in English) | |
| Topics (in Japanese) | (See Japanese page) |
| Topics (in English) | |
| Chair | |
| Vice Chair | |
| Secretary | |
| Assistant | |
| 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) | Development of Control System for Microgravity Experimental System that Uses High Altitude Balloon : Experimental Report and Examination of Pullout Control for Supersonic Flight |
| Sub Title (in English) | |
| Keyword(1) | Microgravity |
| Keyword(2) | Pullout Control |
| Keyword(3) | Supersonic Flight |
| Keyword(4) | Balloon |
| 1st Author's Name | Shouhei KADOOKA |
| 1st Author's Affiliation | Musashi Institute of Technology() |
| 2nd Author's Name | Shujiro SAWAI |
| 2nd Author's Affiliation | Japan Aerospace Exploration Agency, Institute of Space and Astronautical Science |
| 3rd Author's Name | Shin-ichiro SAKAI |
| 3rd Author's Affiliation | Japan Aerospace Exploration Agency, Institute of Space and Astronautical Science |
| 4th Author's Name | Nobutaka BANDO |
| 4th Author's Affiliation | Japan Aerospace Exploration Agency, Institute of Space and Astronautical Science |
| 5th Author's Name | Takehiko ISHIKAWA |
| 5th Author's Affiliation | Japan Aerospace Exploration Agency |
| 6th Author's Name | Tatsuaki HASHIMOTO |
| 6th Author's Affiliation | Japan Aerospace Exploration Agency, Institute of Space and Astronautical Science |
| Date | 2007-11-30 |
| Paper # | SANE2007-82 |
| Volume (vol) | vol.107 |
| Number (no) | 365 |
| Page | pp.pp.- |
| #Pages | 6 |
| Date of Issue | |