Low energy escape trajectory for the Mars moon sample return mission

Makoto Horikawa, Yasuhiro Kawakatsu, Hiroaki Yoshimura

研究成果: Conference contribution

4 被引用数 (Scopus)

抄録

In this paper, we investigate the low-energy escape trajectory design for a mission called Martian Moons eXplorer to achieve the world's first sample return from Martian moon. The hybrid usage of chemical and electric propulsion with combination of the three-body and two-body problems has come into consideration in order to seek a fast low-energy escape from Mars. We first study the needs of pre-departure sequence. Then, we determine the transition point from a low-energy three-body phase to a low-thrust two-body phase, in which the tube dynamics is employed for the low-energy three-body phase. We finally develop charts to reveal the relation between the velocity in Mars Escape Injection maneuver and the required time of flight.

本文言語English
ホスト出版物のタイトルSpaceflight Mechanics 2016
編集者Martin T. Ozimek, Renato Zanetti, Angela L. Bowes, Ryan P. Russell, Martin T. Ozimek
出版社Univelt Inc.
ページ1479-1488
ページ数10
ISBN(印刷版)9780877036333
出版ステータスPublished - 2016
イベント26th AAS/AIAA Space Flight Mechanics Meeting, 2016 - Napa, United States
継続期間: 2016 2月 142016 2月 18

出版物シリーズ

名前Advances in the Astronautical Sciences
158
ISSN(印刷版)0065-3438

Other

Other26th AAS/AIAA Space Flight Mechanics Meeting, 2016
国/地域United States
CityNapa
Period16/2/1416/2/18

ASJC Scopus subject areas

  • 航空宇宙工学
  • 宇宙惑星科学

フィンガープリント

「Low energy escape trajectory for the Mars moon sample return mission」の研究トピックを掘り下げます。これらがまとまってユニークなフィンガープリントを構成します。

引用スタイル