@inproceedings{oai:jaxa.repo.nii.ac.jp:00007300,
 author = {中宮, 賢樹 and 川勝, 康弘 and Simanjuntak, Triwanto and Nakamiya, Masaki and Kawakatsu, Yasuhiro},
 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, Triangular Lagrangian points of the Sun-Jupiter system contains Asteroids which are well known as Trojans. These Asteroids are believed to contain primitive information on the early formation of our Solar System. Furhtermore their origin is also unclear. Considering these significances, we report in this paper mission analysis on the Trojans rendezvous mission using two body approach. The mission design includes the selection of the target Asteroids and the design of the nominal mission sequence. Three types of trajectories are presented, direct transfer, using gravity assists of Mars, Jupiter and also employed low-thrust propulsion to each type in finding reasonable time and DeltaV transfer among selected Asteroids., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0065115053},
 pages = {326--335},
 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 = {Jupiter Trojans Rendezvous Mission Design},
 volume = {20},
 year = {2011}
}