Trajectory options for solar polar region observation mission

Yasuhiro Kawakatsu, Junichiro Kawaguchi

Research output: Contribution to journalArticlepeer-review

Abstract

A study on the post-HINODE Solar Observation Mission has been started by members in the solar physics community. One candidate of the mission targets on the observation of the solar polar region from the orbit largely inclined with the ecliptic plane. In order to achieve this severe mission target, possible trajectory sequences are investigated considering the application of various trajectory manipulation techniques. Three major trajectory options are listed up to achieve the mission objective. The first option, "SEP option", is characterized by the usage of solar electric propulsion (SEP) combined with the earth gravity assists. The other options are characterized by the usage of planetary gravity assists, and SEP is not used in these options. They are named "Jupiter option" and "Venus option" respectively. The comparison among the trajectory options is discussed in the paper, not only from the aspect of the orbital mechanics, but also from the aspects of the spacecraft design and operation.

Original languageEnglish
Pages (from-to)93-103
Number of pages11
JournalJournal of Aerospace Engineering, Sciences and Applications
Volume4
Issue number3
DOIs
Publication statusPublished - 2012 Jul
Externally publishedYes

Keywords

  • Interplanetary Trajectory Design
  • Mission Analysis
  • Out-of-ecliptic Orbit

ASJC Scopus subject areas

  • Aerospace Engineering

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