@inproceedings{oai:jaxa.repo.nii.ac.jp:00007304,
 author = {北嶋, 麻里絵 and 津田, 雄一 and 川口, 淳一郎 and 津田, 慎一 and Kitajima, Maie and Tsuda, Yuichi and Kawaguchi, Junichiro and Tsuda, Shinichi},
 book = {アストロダイナミクスシンポジウム講演後刷り集, The 20th Workshop on JAXA Astrodynamics and Flight Mechanics},
 month = {Mar},
 note = {第20回アストロダイナミクスシンポジウム (2010年7月26-27日. 宇宙航空研究開発機構宇宙科学研究所), 相模原市, 神奈川県, The 20th Workshop on JAXA Astrodynamics and Flight Mechanics 2010 (July 26-27, 2010. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan, 摘要: 地球-火星間の輸送方法は，有人火星探査の実現の鍵を握っている．この課題へのアプローチのひとつとして，"深宇宙港"の利用が挙げられる．深宇宙港とは，太陽－地球ラグランジュ点を建設予定地とし，燃料補給や宇宙船の乗換えを行うという構想である．また惑星間飛行では，多くの物資を輸送できるように，高比推力(低推力)の推進機関が必要となる．, 本研究では，"深宇宙港"及び"低推力推進"の組み合わせを活かした火星往復探査の軌道設計について検討する．, The transportation strategy between Earth and Mars holds the key to the implementation of human exploration mission to Mars. One of the approaches to this problem beyond Earth－Mars direct transfer is a utilization of so-called "Deep Space Port (DSP)" that is a concept of utilizing the Sun-Earth liberation points for refueling and cargo handover for interplanetary transportation. Furthermore, the interplanetary transfer requires high specific impulse (with low thrust practically) to transport as much payload as possible., In this paper, we discuss the transportation architecture for the round-trip exploration to Mars taking advantage of the combination of the "DSP" and "low-thrust propulsion."., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0065115057},
 pages = {357--362},
 publisher = {宇宙航空研究開発機構宇宙科学研究所 (JAXA)(ISAS), Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)},
 title = {A Study on Trajectory for Round-trip Exploration to Mars Utilizing Deep Space Port at Sun-Earth L2 point},
 volume = {20},
 year = {2011}
}