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ガスジェットによる大型ゴンドラの方向制御
https://jaxa.repo.nii.ac.jp/records/33017
https://jaxa.repo.nii.ac.jp/records/3301750ad2fa1-c7b2-4f01-a210-d5c6e6d69bfd
名前 / ファイル | ライセンス | アクション |
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SA0166861.pdf (929.5 kB)
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Item type | 紀要論文 / Departmental Bulletin Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | ガスジェットによる大型ゴンドラの方向制御 | |||||
言語 | ||||||
言語 | jpn | |||||
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 | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Side-jet Azimuth Control System for Large Balloon Gondola | |||||
著者 |
矢島, 信之
× 矢島, 信之× 太田, 茂雄× 秋山, 弘光× 岡部, 選司× 西村, 純× 橋本, 保成× 川口, 淳一郎× YAJIMA, Nobuyuki× OHTA, Shigeo× AKIYAMA, Hiromitsu× OKABE, Yorigi× NISHIMURA, Jun× HASHIMOTO, Yasunari× KAWAGUCHI, Junichiro |
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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 |
宇宙科学研究所報告. 特集: 大気球研究報告 巻 22, p. 27-42, 発行日 1988-11 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | An azimuth control system using N_2 gas thruster (S-J control system) has been developed and employed for the quick and steady control of a large and heavy balloon gondola. In the gondola, a winged space vehicle and a booster rocket are to be installed for its re-entry flight test. When the balloon reaches ceiling altitude, the gondola is oriented to the required direction by using the S-J control system and then the vehicle is released from the gondola. A preliminary flight test has been carried out to test the S-J control system and a separation mechanism of the vehicle at Sanriku Balloon Center in May 1987. The experimental results show that this control system is applicable for the actual re-entry flight test of the winged space vehicle. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0285-9920 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN00354485 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: SA0166861000 |