Escape trajectories for martian moons explorer using chemical and electric propulsion

Makoto Horikawa, Takanao Saiki, Yasuhiro Kawakatsu, Hiroaki Yoshimura

    研究成果: Conference contribution

    2 引用 (Scopus)

    抄録

    This work discusses on designing fast and efficient Mars escape trajectory for Martian Moons eXplorer in the three-body system using chemical and electric propulsion. Chemical propulsion is used for fast low-energy escape from Mars and electric propulsion is used to increase v-infinity and to re-encounter with Mars for a gravity assist. We propose a method called “all-three-body method" and we compare the new method with the patched three-and-two-body method, and a parametric study is carried out. Using electric propulsion soon after Mars escape injection done by chemical propulsion, the all-three-body method would consume less fuel than patched three-and-two-body method. Limiting the use of chemical propulsion could also increase the final spacecraft mass when electric propulsion is used within 10 days after impulsive maneuver.

    元の言語English
    ホスト出版物のタイトルAIAA/AAS Astrodynamics Specialist Conference, 2016
    出版者American Institute of Aeronautics and Astronautics Inc, AIAA
    ISBN(印刷物)9781624104459
    出版物ステータスPublished - 2016
    イベントAIAA/AAS Astrodynamics Specialist Conference, 2016 - Long Beach, United States
    継続期間: 2016 9 132016 9 16

    Other

    OtherAIAA/AAS Astrodynamics Specialist Conference, 2016
    United States
    Long Beach
    期間16/9/1316/9/16

    Fingerprint

    chemical propulsion
    electric propulsion
    Electric propulsion
    Moon
    natural satellites
    escape
    mars
    Trajectories
    trajectories
    Propulsion
    Spacecraft
    maneuvers
    Gravitation
    propulsion
    encounters
    infinity
    spacecraft
    injection
    gravitation

    ASJC Scopus subject areas

    • Astronomy and Astrophysics
    • Aerospace Engineering

    これを引用

    Horikawa, M., Saiki, T., Kawakatsu, Y., & Yoshimura, H. (2016). Escape trajectories for martian moons explorer using chemical and electric propulsion. : AIAA/AAS Astrodynamics Specialist Conference, 2016 American Institute of Aeronautics and Astronautics Inc, AIAA.

    Escape trajectories for martian moons explorer using chemical and electric propulsion. / Horikawa, Makoto; Saiki, Takanao; Kawakatsu, Yasuhiro; Yoshimura, Hiroaki.

    AIAA/AAS Astrodynamics Specialist Conference, 2016. American Institute of Aeronautics and Astronautics Inc, AIAA, 2016.

    研究成果: Conference contribution

    Horikawa, M, Saiki, T, Kawakatsu, Y & Yoshimura, H 2016, Escape trajectories for martian moons explorer using chemical and electric propulsion. : AIAA/AAS Astrodynamics Specialist Conference, 2016. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA/AAS Astrodynamics Specialist Conference, 2016, Long Beach, United States, 16/9/13.
    Horikawa M, Saiki T, Kawakatsu Y, Yoshimura H. Escape trajectories for martian moons explorer using chemical and electric propulsion. : AIAA/AAS Astrodynamics Specialist Conference, 2016. American Institute of Aeronautics and Astronautics Inc, AIAA. 2016
    Horikawa, Makoto ; Saiki, Takanao ; Kawakatsu, Yasuhiro ; Yoshimura, Hiroaki. / Escape trajectories for martian moons explorer using chemical and electric propulsion. AIAA/AAS Astrodynamics Specialist Conference, 2016. American Institute of Aeronautics and Astronautics Inc, AIAA, 2016.
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