Escape trajectories from the L2 point of the earth-moon system

Keita Tanaka, Jun'Ichiro Kawaguchi

研究成果: Article査読

抄録

To use the L2 point of the Earth-Moon (EM) system as a space transportation hub, it is absolutely necessary to know the available orbital energy of a spacecraft departing from EM L2 and how to obtain required excess velocity to the target planet. This paper presents a successful acceleration strategy using the combination of an impulsive maneuver and the Sun gravitational perturbation. Applying this strategy enables the spacecraft to efficiently convert the energy of the maneuver into its orbital energy.

本文言語English
ページ(範囲)238-244
ページ数7
ジャーナルTransactions of the Japan Society for Aeronautical and Space Sciences
57
4
DOI
出版ステータスPublished - 2014 7
外部発表はい

ASJC Scopus subject areas

  • 航空宇宙工学
  • 宇宙惑星科学

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