High velocity aero-gravity assist applied on eccentricity to inclination conversion for reaching solar polar orbit

Tiago Monteiro Padovan, Yuki Kubo, Junichiro Kawaguchi, Kazuhiko Yamada, Roger Gutierrez Ramon

研究成果: Conference contribution

抄録

In order to change the inclination of an orbit around the Sun, a good option is to perform a flyby on Jupiter, where heliocentric speeds are slower than in the inner solar system. The drawback of the resulting orbit is the great orbital period associated with its large semi-major axis. In order to reduce the orbit size and increase even more the inclination, it was suggested to implement an Aero-gravity Assist maneuver at the Earth after the Jupiter flyby. This maneuver would be used within the Eccentricity to Inclination conversion scheme to increase its performance. Results show that such a maneuver could reduce the time required for reaching a short period, highly inclined orbit in lower time than by only using Gravity Assist. The objective of this study is to analyze the performance of using Aero-gravity Assist within the Eccentricity to Inclination conversion.

本文言語English
ホスト出版物のタイトルAIAA Scitech 2020 Forum
出版社American Institute of Aeronautics and Astronautics Inc, AIAA
ページ1-7
ページ数7
ISBN(印刷版)9781624105951
DOI
出版ステータスPublished - 2020
外部発表はい
イベントAIAA Scitech Forum, 2020 - Orlando, United States
継続期間: 2020 1 62020 1 10

出版物シリーズ

名前AIAA Scitech 2020 Forum
1 PartF

Conference

ConferenceAIAA Scitech Forum, 2020
国/地域United States
CityOrlando
Period20/1/620/1/10

ASJC Scopus subject areas

  • 航空宇宙工学

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