| Paper Abstract and Keywords |
| Presentation |
2007-11-30 10:20
Development of Control System for Microgravity Experiment System that Uses High Altitude Balloon
-- Experimental Report and Examination of Pullout Control for Supersonic Flight -- Shouhei Kadooka (MI-tech), Shujiro Sawai, Shin-ichiro Sakai, Nobutaka Bando, Takehiko Ishikawa, Tatsuaki Hashimoto (JAXA・ISAS) SANE2007-82 |
| Abstract |
(in Japanese) |
(See Japanese page) |
| (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 40 km 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) |
| (in English) |
Microgravity / Pullout Control / Supersonic Flight / Balloon / / / / |
| Reference Info. |
IEICE Tech. Rep., vol. 107, no. 365, SANE2007-82, pp. 1-6, Nov. 2007. |
| Paper # |
SANE2007-82 |
| Date of Issue |
2007-11-23 (SANE) |
| ISSN |
Print edition: ISSN 0913-5685 Online edition: ISSN 2432-6380 |
Copyright and reproduction |
All rights are reserved and no part of this publication may be reproduced or transmitted in any form or by any means, electronic or mechanical, including photocopy, recording, or any information storage and retrieval system, without permission in writing from the publisher. Notwithstanding, instructors are permitted to photocopy isolated articles for noncommercial classroom use without fee. (License No.: 10GA0019/12GB0052/13GB0056/17GB0034/18GB0034) |
| Download PDF |
SANE2007-82 |
| Conference Information |
| Committee |
SANE |
| Conference Date |
2007-11-30 - 2007-11-30 |
| Place (in Japanese) |
(See Japanese page) |
| Place (in English) |
ISAS,JAXA (Sagamihara) |
| Topics (in Japanese) |
(See Japanese page) |
| Topics (in English) |
Sensing and measurement of space, and general |
| Paper Information |
| Registration To |
SANE |
| Conference Code |
2007-11-SANE |
| Language |
Japanese |
| Title (in Japanese) |
(See Japanese page) |
| Sub Title (in Japanese) |
(See Japanese page) |
| Title (in English) |
Development of Control System for Microgravity Experiment System that Uses High Altitude Balloon |
| Sub Title (in English) |
Experimental Report and Examination of Pullout Control for Supersonic Flight |
| Keyword(1) |
Microgravity |
| Keyword(2) |
Pullout Control |
| Keyword(3) |
Supersonic Flight |
| Keyword(4) |
Balloon |
| Keyword(5) |
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| Keyword(6) |
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| Keyword(8) |
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| 1st Author's Name |
Shouhei Kadooka |
| 1st Author's Affiliation |
Musashi Institute of Technology (MI-tech) |
| 2nd Author's Name |
Shujiro Sawai |
| 2nd Author's Affiliation |
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science (JAXA・ISAS) |
| 3rd Author's Name |
Shin-ichiro Sakai |
| 3rd Author's Affiliation |
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science (JAXA・ISAS) |
| 4th Author's Name |
Nobutaka Bando |
| 4th Author's Affiliation |
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science (JAXA・ISAS) |
| 5th Author's Name |
Takehiko Ishikawa |
| 5th Author's Affiliation |
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science (JAXA・ISAS) |
| 6th Author's Name |
Tatsuaki Hashimoto |
| 6th Author's Affiliation |
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science (JAXA・ISAS) |
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| Speaker |
Author-1 |
| Date Time |
2007-11-30 10:20:00 |
| Presentation Time |
25 minutes |
| Registration for |
SANE |
| Paper # |
SANE2007-82 |
| Volume (vol) |
vol.107 |
| Number (no) |
no.365 |
| Page |
pp.1-6 |
| #Pages |
6 |
| Date of Issue |
2007-11-23 (SANE) |