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On the Simulation Test for the Relative Motion of Separated Sub-Boosters on M-3SII with Nearly Half a Model Vehicle ST-735 and their Motion Analyses Using Inertial Sensors Output
https://jaxa.repo.nii.ac.jp/records/31401
https://jaxa.repo.nii.ac.jp/records/31401f00eb5a6-c4c7-4588-95a6-034fcc3f2777
| 名前 / ファイル | ライセンス | アクション |
|---|---|---|
SA0035086.pdf (951.7 kB)
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| Item type | 紀要論文 / Departmental Bulletin Paper(1) | |||||||
|---|---|---|---|---|---|---|---|---|
| 公開日 | 2015-03-26 | |||||||
| タイトル | ||||||||
| タイトル | On the Simulation Test for the Relative Motion of Separated Sub-Boosters on M-3SII with Nearly Half a Model Vehicle ST-735 and their Motion Analyses Using Inertial Sensors Output | |||||||
| 言語 | en | |||||||
| 言語 | ||||||||
| 言語 | eng | |||||||
| 資源タイプ | ||||||||
| 資源タイプ識別子 | http://purl.org/coar/resource_type/c_6501 | |||||||
| 資源タイプ | departmental bulletin paper | |||||||
| 著者 |
TSUKAMOTO, Shigeki
× TSUKAMOTO, Shigeki
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| 出版者 | ||||||||
| 出版者 | 宇宙科学研究所 | |||||||
| 出版者（英） | ||||||||
| 出版者 | Institute of Space and Astronautical Science | |||||||
| 書誌情報 |
en : The Institute of Space and Astronautical Science report 巻 635, p. 1-15, 発行日 1989-02 |
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| 抄録（英） | ||||||||
| 内容記述タイプ | Other | |||||||
| 内容記述 | In the course of development for M-3SII type vehicle which has two relatively large sub-boosters, a possibility of collision between the separated sub-booster and the core-motor was discussed with concern especially in relation to the effect of the core-motor plume. We had a flight simulation test under the conditions specified by the similarity law given in this paper with ST-735,nearly half a scale model of M-3SII, and the relative motion of the sub-booster was analyzed with on board TV, inertial sensors and a measuring device of separation distance. Althouhg TV pictures provide us with real time, high speed images of the sub-booster, only 2 dimensional information is obtained in principle. Analysis on the motion with 12 inertial sensors informs us of a complete 3 dimensional motion of the sub-booster. We could predict from the test that the exhaust plume would not influence on the motion of the separated sub-boosters in M-3SII flight. | |||||||
| ISSN | ||||||||
| 収録物識別子タイプ | ISSN | |||||||
| 収録物識別子 | 0285-6808 | |||||||
| 書誌レコードID | ||||||||
| 収録物識別子タイプ | NCID | |||||||
| 収録物識別子 | AA10632072 | |||||||
| 資料番号 | ||||||||
| 内容記述タイプ | Other | |||||||
| 内容記述 | 資料番号: SA0035086000 | |||||||
