Preliminary Mission Analysis and Orbit Design for Next Mars Exploration

DOI Web Site 被引用文献1件
  • OGAWA Naoko
    JAXA Space Exploration Center, Japan Aerospace Exploration Agency
  • Y. MORIMOTO Mutsuko
    JAXA Space Exploration Center, Japan Aerospace Exploration Agency
  • TSUDA Yuichi
    JAXA Space Exploration Center, Japan Aerospace Exploration Agency Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
  • YAMADA Tetsuya
    JAXA Space Exploration Center, Japan Aerospace Exploration Agency Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
  • FUJITA Kazuhisa
    JAXA Space Exploration Center, Japan Aerospace Exploration Agency Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency
  • YAMAGUCHI Tomohiro
    The Graduate University for Advanced Studies
  • KAWAKATSU Yasuhiro
    JAXA Space Exploration Center, Japan Aerospace Exploration Agency Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
  • KUBOTA Takashi
    JAXA Space Exploration Center, Japan Aerospace Exploration Agency Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
  • KAWAGUCHI Jun'ichiro
    JAXA Space Exploration Center, Japan Aerospace Exploration Agency Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency

抄録

Japan has launched many interplanetary spacecraft for exploration of solar system bodies including Mars. Now we are planning the next Mars mission in the late 2010's. This paper describes the preliminary mission analysis and orbit design for this plan. The combined exploration by several spacecraft requires complicated and careful consideration, different from those for single-probe missions. Mission plans to realize required configuration by a single launch and simple simulation results are reported.

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