@inproceedings{oai:jaxa.repo.nii.ac.jp:00007579,
 author = {石井, 信明 and 山川, 宏 and Ishii, Nobuaki and Yamakawa, Hiroshi},
 book = {第15回アストロダイナミクスシンポジウム講演後刷り集　2005, Proceedings of 15th Workshop on JAXA Astrodynamics and Flight Mechanics},
 month = {Mar},
 note = {現在、金星探査機(PLANET-C: Venus Climate Orbiter)は2010年打上げを前提に、ミッション解析が進められている。軌道計画の実現性を確認する目的で、打上げ直後の第1可視運用性、金星周回軌道中の日陰時間、探査機に要求される燃料重量などを算出し、探査機システムとの整合性を確認した。本稿では、これら2010年打上げ軌道の特徴と現状における打上げウィンドウを示す。, In the present study, the launch windows in May and June, 2010 are applied to the PLANET-C (Venus Climate Orbiter) Venus exploring mission. So as to verify the system compatibility between the orbital design and the spacecraft capability, antenna elevation in the first visible pass from UDSC (Usuda Deep Space Center) and shadow duration of the elliptic orbit about Venus are evaluated in this paper. Required velocity amount for orbit and attitude correction is also estimated for the 2010 launch orbit. Currently, three weeks in total of launch possibilities, one week in May and two weeks in June 2010, are ensured for the PLANET-C mission., 資料番号: AA0063480014},
 pages = {86--91},
 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/ISAS)},
 title = {Orbital characteristics of Venus explorer, PLANET-C},
 year = {2006}
}