JAXA Repository / AIREX 未来へ続く、宙(そら)への英知
Other TitleDevelopment and evaluation flight test results of a controlled-descent type payload system optimized for the recovery from a very small balloon
Author(jpn)平塚, 丘将; 河野, 紘基; 山本, 真行
Author(eng)Hiratsuka, Takamasa; Kono, Hiroki; Yamamoto, Masayuki
Author Affiliation(jpn)高知工科大学; 高知工科大学; 高知工科大学
Author Affiliation(eng)Kochi University of Technology; Kochi University of Technology; Kochi University of Technology
Issue Date2017-03-14
Japan Aerospace Exploration Agency (JAXA)
Publication title宇宙航空研究開発機構研究開発報告: 大気球研究報告
JAXA Research and Development Report
Start page81
End page100
Publication date2017-03-14
In order to solve some difficulties on the balloon recovery system with a conventional parachute, a recovery system with a parafoil for the controlled-descent was designed and basic on-board system was developed for the real flight operation in near future. Simulating flights from small balloons, six flight tests from an aerial vehicle were carried out to evaluate its capability of the trajectory control and to measure its short term gliding ratio. Through the series of the tests, the system was validated and the averaged short term gliding ratio for about 5 s was measured to be larger than 3.
Description形態: カラー図版あり
Physical characteristics: Original contains color illustrations
Document TypeTechnical Report
JAXA Category研究開発報告
NASA Subject CategoryAircraft Design, Testing and Performance
Report NoJAXA-RR-16-008

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