University of Tokyo's CubeSat Project - Mission Concept and Subsystem Design -

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This paper describes outline of the University of Tokyo Intelligent Space Systems Laboratory(ISSL)'s CubeSat "XI" for the demonstration of the pico-satellite bus technology and validation of the commercial-off-the-shelf parts in space as well as the earth imaging mission. CubeSat project is the international joint program, which aims for developing and actually launching 10cm cubic satellites weighing less than 1kg to the earth's orbit. 18 CubeSats developed by Japanese and U.S. institutes are to be launched by the Russian launch vehicle "Dnepr" in Nowember 2002 to the Sun-synchronized orbit. The project in ISSL is conducted by 20 space engineering students as a material of education.

収録刊行物

  • The Journal of space technology and science : a publication of Japanese Rocket Society

    The Journal of space technology and science : a publication of Japanese Rocket Society 16(1), 37-46, 2000-03-01

    Japanese Rocket Society

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各種コード

  • NII論文ID(NAID)
    10008495084
  • NII書誌ID(NCID)
    AA10925183
  • 本文言語コード
    ENG
  • 資料種別
    ART
  • ISSN
    0911551X
  • データ提供元
    CJP書誌  CJP引用  J-STAGE 
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