書誌事項
- タイトル別名
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- ガス ジェット ニ ヨル オオガタ ゴンドラ ノ ホウコウ セイギョ
- Side-jet Azimuth Control System for Large Balloon Gondola
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説明
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.
資料番号: SA0166861000
収録刊行物
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- 宇宙科学研究所報告. 特集: 大気球研究報告
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宇宙科学研究所報告. 特集: 大気球研究報告 22 27-42, 1988-11
宇宙科学研究所
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詳細情報 詳細情報について
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- CRID
- 1050566774915261568
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- NII論文ID
- 110000222815
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- NII書誌ID
- AN00354485
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- ISSN
- 02859920
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- NDL書誌ID
- 3203114
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- 本文言語コード
- ja
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- 資料種別
- departmental bulletin paper
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- データソース種別
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- IRDB
- NDL
- CiNii Articles
