Results of Microgravity Experiments Using the Balloon Operated Vehicle with a New Drag-Free Control Method

DOI:10.15011/ijmsa.32.320211
Int. J. Microgravity Sci. Appl. 2015p320211
論文著者
M. KIKUCHI, T. ISHIKAWA, S. YAMAMOTO, S. SAWAI, Y. MARU, S. SAKAI, N. BANDO, S. SHIMIZU,H. KOBAYASHI, T. YOSHIMITSU, Y. KAN, T. MIZUSHIMA, S. FUKUYAMA, J. OKADA,S. YODA, H. FUKE, Y. KAKEHASHI and T. HASHIMOTO
所属組織
Japan Aerospace Exploration Agency (JAXA), IIC Co. Ltd., A.E.S. Co. Ltd.
要約
A microgravity experiment system using a high altitude balloon has been developed. In order to accommodate payloads larger than previous system which employed three- dimensional drag-free control, one-dimensional drag-free control has been applied. The first test flight was conducted in Aug. 2014. A gravity level below 10-3 G was obtained for more than 30 seconds during the free-fall of the capsule. A combustion experiment was conducted during the low gravity condition.
Keyword(s)
High altitude balloon, Free-fall, Drag-free control
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Received 25 Dec. 2014, accepted 26 Feb. 2015, published 31 Apr. 2015

© The Japan Society of Microgravity Applicaiton

この投稿文は次の言語で読めます: 英語

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