NEC Aerospace Systems
NEC Aerospace Systems
NEC Aerospace Systems
NEC Aerospace Systems
NEC Aerospace Systems
NEC Aerospace Systems
Japan Aerospace Exploration Agency (JAXA)
Japan Aerospace Exploration Agency (JAXA)
Japan Aerospace Exploration Agency (JAXA)
Japan Aerospace Exploration Agency (JAXA)
Japan Aerospace Exploration Agency (JAXA)
Japan Aerospace Exploration Agency (JAXA)
出版者
宇宙航空研究開発機構宇宙科学研究本部
出版者（英）
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)
雑誌名
アストロダイナミクスシンポジウム講演後刷り集
雑誌名(英)
Proceedings of 18th workshop on JAXA Astrodynamics and flight mechanics
巻
2008
発行年
2009-03
会議概要（会議名, 開催地, 会期, 主催者等）（英）
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
KAGUYA (SELENE) is Japan's first large lunar explorer that was launched on September 14, 2007 by the H-IIA launch vehicle. We selected a phasing lunar transfer orbit with 2 loops as the KAGUYA lunar transfer orbit and six series of lunar insertion maneuvers. Then, KAGUYA was inserted into the orbit around the Moon with decelerating maneuver on October 3, 2007 that was called Lunar Orbit Insertion 1(LOI1). After that, KAGUYA conducted decelerating maneuvers several times at the perilune and gradually decreased apolune height. In this process, KAGUYA separated Rstar and Vstar. Finally, it was inserted into the observation orbit, which was the circular orbit with 100km of height and 90 degrees of orbital inclination on October 18, 2007. This paper represents the KAGUYA's orbital maneuver plans and shows the operational results during lunar transfer orbit and lunar orbit insertion.
内容記述
形態: カラー図版あり
著者人数: 14人
内容記述（英）
Physical characteristics: Original contains color illustrations
「かぐや（SELENE）」の月遷移軌道と月周回軌道投入における軌道制御計画および運用結果
