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  [in Japanese] Development and Flight Experiment Results of Microgravity Experiment System with One-Directional Drag-Free Control using High Altitude Balloon  [in Japanese]

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Author(s)

Abstract

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.

Journal

  • JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES

    JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 63(6), 257-264, 2015

    THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES

Codes

  • NII Article ID (NAID)
    130005112407
  • NII NACSIS-CAT ID (NCID)
    AA11307372
  • Text Lang
    JPN
  • ISSN
    1344-6460
  • NDL Article ID
    026984223
  • NDL Call No.
    Z74-B503
  • Data Source
    NDL  J-STAGE 
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