On ultimately the most highly inclined, the most concise solar polar trajectory with practically the shortest period

研究成果: Conference contribution

抄録

This paper presents the extended orbital synthesis results from the author’s work in 2009 to achieve ballistic and short period out-of-ecliptic trajectories which possess ultimately the most highly and most concise solar polar properties. Those are realized through almost ballistic flight instead of using electric propulsion or solar sail acceleration. The strategy developed utilizes a Jovian gravity assist first, followed by very high speed synchronized multiple polar gravity assists by Earth or Venus. While the author’s work in 2009 presented the trajectories down to almost one year period, this paper will present the further sequences that make the semi-major axis lower than one AU and lower the perihelion distance closer to the Sun for close-up observation of the Sun.

本文言語English
ホスト出版物のタイトル1st IAA/AAS SciTech Forum on Space Flight Mechanics and Space Structures and Materials, 2018
編集者Yury N. Razoumny, Filippo Graziani, Anna D. Guerman, Jean-Michel Contant
出版社Univelt Inc.
ページ53-61
ページ数9
ISBN(印刷版)9780877036630
出版ステータスPublished - 2020
外部発表はい
イベント1st IAA/AAS SciTech Forum on Space Flight Mechanics and Space Structures and Materials, 2018 - Moscow, Russian Federation
継続期間: 2018 11 132018 11 15

出版物シリーズ

名前Advances in the Astronautical Sciences
170
ISSN(印刷版)0065-3438

Conference

Conference1st IAA/AAS SciTech Forum on Space Flight Mechanics and Space Structures and Materials, 2018
国/地域Russian Federation
CityMoscow
Period18/11/1318/11/15

ASJC Scopus subject areas

  • 航空宇宙工学
  • 宇宙惑星科学

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