On earth-moon transfer trajectory with gravitational capture

Hiroshi Yamakawa, Jun'ichiro Kawaguchi, NObuaki Ishii, Hiroki Matsuo

Research output: Chapter in Book/Report/Conference proceedingConference contribution

51 Citations (Scopus)

Abstract

Approaching from outside the sphere of influence, a particle may attain low relative velocity was a celestial body and even rotate around it temporarily, without utilizing any other effects than gravitational force. This mechanism is called gravitational capture (i.e. ballistic capture) and it has been considered to be one of the mechanisms which can explain the origin of planetary satellites. In astrodynamics field, lunar gravitational capture is applied to earth-moon transfer trajectory along with positive use of solar perturbation, paying attention to small delta-V required at lunar orbit insertion. In this paper, from the viewpoint of local two-body energy variation, the mechanism of gravitational capture is analytically investigated. Furthermore, a systematic design method for earth-moon transfer trajectory followed by gravitational capture is established.

Original languageEnglish
Title of host publicationAdvances in the Astronautical Sciences
PublisherPubl by Univelt Inc
Pages397-416
Number of pages20
Editionpt 1
ISBN (Print)0877033803
Publication statusPublished - 1993
Externally publishedYes
EventProceedings of the AAS/AIAA Astrodynamics Conference. Part 3 (of 3) - Victoria, BC, Can
Duration: 1993 Aug 161993 Aug 19

Publication series

NameAdvances in the Astronautical Sciences
Numberpt 1
Volume85
ISSN (Print)0065-3438

Conference

ConferenceProceedings of the AAS/AIAA Astrodynamics Conference. Part 3 (of 3)
CityVictoria, BC, Can
Period93/8/1693/8/19

ASJC Scopus subject areas

  • Aerospace Engineering
  • Space and Planetary Science

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