日本航空宇宙学会論文集
Online ISSN : 2432-3691
Print ISSN : 1344-6460
ISSN-L : 1344-6460
論文
気球を利用した微小重力実験のための,一軸制御型機体システムの 開発と飛行実験結果
丸 祐介石川 毅彦坂東 信尚澤井 秀次郎清水 成人坂井 真一郎吉光 徹雄小林 弘明菊池 政雄山本 信福山 誠二郎岡田 純平菅 勇志梯 友哉福家 英之伊藤 琢博水島 隆成江口 光
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2015 年 63 巻 6 号 p. 257-264

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In this paper is presented a microgravity experiment system utilizing a high altitude balloon. The feature is a double shell structure of a vehicle that is dropped off from the balloon and a microgravity experiment section that is attached to the inside of the vehicle with a liner slider. Control with cold gas jet thrusters of relative position of the experiment section to the vehicle and attitude of the vehicle maintains fine microgravity environment. The design strategy of the vehicle is explained, mainly referring to differences from the authors' previous design. The result of the flight experiment is also shown to evaluate the characteristics of the presented system.

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© 2015 The Japan Society for Aeronautical and Space Sciences
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