@inproceedings{oai:jaxa.repo.nii.ac.jp:00007323,
 author = {川口, 淳一郎 and 川勝, 康弘 and 森本, 睦子 and Kawaguchi, Junichiro and Kawakatsu, Yasuhiro and Morimoto, Mutsuko Y. and Atchison, Justin A.},
 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 19th workshop on JAXA Astrodynamics and Flight Mechanics},
 month = {Mar},
 note = {アストロダイナミクスシンポジウム (2009年7月30-31日. 宇宙航空研究開発機構宇宙科学研究本部)), Workshop on JAXA Astrodynamics and Flight Mechanics, 2009 (July 30-31, 2009. Institute of Space and Astronautical Science (ISAS), Japan Aerospace Exploration Agency (JAXA)), Sagamihara, Kanagawa Japan, 本論文は，純弾道飛行にて，短周期の対黄道面高傾斜角軌道を実現する手法について，とくに木星を利用する場合について述べる．, This paper presents new orbital synthesis results to achieve ballistic and short period out-of ecliptic trajectories, instead of using electric propulsion or solar sail acceleration. The strategy developed utilizes a Jovian gravity first, followed by polar very high speed gravity assists by Earth or Venus. So far, the use of very high speed gravity assists has been conceived not practically useful. However, this paper presents those still effectively contribute to amending the trajectories periods, and to acquiring small sized out-of-ecliptic ballistic trajectories. The biggest advantage of this strategy is to reduce propellant mass carried drastically., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0064734018},
 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 = {ON BALLISTIC ACQUISITION OF SHORT PERIOD OUT-OF-ECLIPTIC TRAJECTORIES},
 volume = {2009},
 year = {2010}
}