Short-period ballistic out-of-ecliptic trajectories via multiple venus & earth swing-bys and vega-driven multiple earth swing-bys

Jun'ichiro Kawaguchi, Michihiro Matsumoto

研究成果: Conference contribution

抄録

This paper presents a few alternative, still ballistic, realization of short-period and highly inclined orbits by utilizing Venus and Earth swing-bys. This paper presents therefore different new approaches. The use of VEGA (Venus-Earth Gravity Assist) strategy lowers the departure escape velocity from Earth. The initial escape v-infmity velocity is only 4.2 km/sec and the strategy enables 37 degrees inclination with respect to the ecliptic plane. At the same time, the paper presents also a derivative strategy, co-use of Delta-VEGA (Delta-V Earth Gravity Assist) strategy for shorter realization. The results are amazing and significantly relaxes the propulsion requirement enhancing the payload mass in comparison with what was shown last year.

本文言語English
ホスト出版物のタイトル61st International Astronautical Congress 2010, IAC 2010
ページ531-538
ページ数8
出版ステータスPublished - 2010
外部発表はい
イベント61st International Astronautical Congress 2010, IAC 2010 - Prague, Czech Republic
継続期間: 2010 9 272010 10 1

出版物シリーズ

名前61st International Astronautical Congress 2010, IAC 2010
1

Other

Other61st International Astronautical Congress 2010, IAC 2010
国/地域Czech Republic
CityPrague
Period10/9/2710/10/1

ASJC Scopus subject areas

  • 航空宇宙工学
  • 天文学と天体物理学

フィンガープリント

「Short-period ballistic out-of-ecliptic trajectories via multiple venus & earth swing-bys and vega-driven multiple earth swing-bys」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