JAXA Repository / AIREX 未来へ続く、宙(そら)への英知

There are no files associated with this item.

Other TitleConceptual study of a Titan atmosphere entry probe
Author(jpn)奥山 圭一; 山田 哲哉; 加藤 純郎
Author(eng)Okuyama, Keiichi; Yamada, Tetsuya; Kato, Sumio
Author Affiliation(jpn)川崎重工業; 宇宙航空研究開発機構 宇宙科学研究本部; 川崎重工業
Author Affiliation(eng)Kawasaki Heavy Industries Ltd.; Japan Aerospace Exploration Agency Institute of Space and Astronautical Science; Kawasaki Heavy Industries Ltd.
Issue Date2005-03
PublisherInstitute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)
Publication title宇宙航行の力学シンポジウム 平成16年度
Symposium on Flight Mechanics and Astrodynamics 2004
Start page29
End page32
Publication date2005-03
KeywordsTitan; satellite atmosphere; space exploration; aerodynamic heating; atmospheric entry; CFRP; ablator; heat shielding; タイタン; 衛星大気; 宇宙探査; 空力加熱; 大気圏突入; CFRP; アブレータ; 熱シールド
Document TypeConference Paper
JAXA Categoryシンポジウム・研究会

Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.