Tether cutting maneuver in swing-by trajectory

Tsubasa Yamasaki, Mai Bando, Shinji Hokamoto

Research output: Contribution to journalArticle

Abstract

The swing-by maneuver is known as a method to change the velocity of a spacecraft by using the gravity force of the celestial body. The powered swing-by has been studied to enhance the velocity change during the swing-by maneuver. This paper studies another way of the powered swing-by using tether cutting, which does not require additional propellant consumption, and shows that the proposed powered swing-by can increase the effect of the swing-by as same as using impulsive thrust. Moreover, it is discussed whether the system has possibility to realize both the powered swing-by of a mother satellite and the planetary capture of a subsatellite simultaneously.

Original languageEnglish
Pages (from-to)212-220
Number of pages9
JournalActa Astronautica
Volume142
DOIs
Publication statusPublished - Jan 1 2018

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Tetherlines
Trajectories
Propellants
Spacecraft
Gravitation
Satellites

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering

Cite this

Tether cutting maneuver in swing-by trajectory. / Yamasaki, Tsubasa; Bando, Mai; Hokamoto, Shinji.

In: Acta Astronautica, Vol. 142, 01.01.2018, p. 212-220.

Research output: Contribution to journalArticle

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