@inproceedings{oai:jaxa.repo.nii.ac.jp:00007402,
 author = {芝崎, 裕介 and 船瀬, 龍 and 津田, 雄一 and 川口, 淳一郎 and Shibasaki, Yusuke and Funase, Ryu and Tsuda, Yuichi and Kawaguchi, Junichiro},
 book = {アストロダイナミクスシンポジウム講演後刷り集, Proceedings of 18th workshop on JAXA Astrodynamics and flight mechanics},
 month = {Mar},
 note = {Symposium on Flight Mechanics and Astrodynamics 2008 (July 28-29, 2008. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)), Sagamihara, Kanagawa Japan, 摘要: この研究では,月低軌道と地球低軌道間を運行すると想定される軌道間輸送機(OTV)の軌道変換について論じている.とくに,電気推進機関などの高効率の推進機関のよる軌道変換の得失を述べ.併せてエアロブレーキングによる軌道換作のメリットを議論し,その結果を述べている., This paper discusses the orbital sequences in Orbital Transfer Vehicle(OTV) assumed operated between Low Lunar Orbit(LLO) and Low Earth orbit(LEO). The fundamental orbit amendment strategies are studied and summarized with the benefit in the use of Aerobraking strategy. The paper discusses the advantage in the use of high efficiency electronic propulsion elements against that in conventional chemical propulsion system., 資料番号: AA0064733028},
 publisher = {宇宙航空研究開発機構宇宙科学研究本部, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)},
 title = {Optimization of Return Trajectories for Orbital Transfer Vehicle between Earth and Moon},
 volume = {2008},
 year = {2009}
}