Výsledky vyhledávání - "宇宙カプセル"

Technology improvement in assessment of planetary entry environments and prediction of thermal protection system performance

Autor: Fujita, Kazuhisa, Matsuyama, Shingo, Suzuki, Toshiyuki, Matsukawa, Yutaka

Publikováno v: 宇宙航空研究開発機構特別資料: 平成18年度宇宙航空研究開発機構総合技術研究本部宇宙科学研究本部研究成果報告書 = JAXA Special Publication: Report on Research Achievements for FY2006 Institute of Space and Astronautical Science, Institute of Aerospace Technology, Japan Aerospace Exploration Agency. :103-106

Comprehensive researches on high-enthalpy flows and associated thermal protection technologies have been conducted in Aerodynamic Research Group, IAT, in cooperation with other research groups in JAXA. In this article, an over-view and the current st

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::5ba721af934d139484dcd4b7ba2ab46a
http://id.nii.ac.jp/1696/00006000/

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High enthalpy aerodynamic heating experiments over a reentry capsule

Autor: Hashimoto, Tokitada, Komuro, Tomoyuki, Takahashi, Masahiro, Sato, Kazuo, Ito, Katsuhiro

In recent years, development of re-usable space transportation system is promoted. However, in order to realize it, development of the base technology is indispensable, particularly, aerodynamic heating and characteristics with strong real gas phenom

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http://id.nii.ac.jp/1696/00005997/

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Attitude movement of a USERS capsule at reentry

Autor: Matsuda, Seiji, Hiraki, Koju, Abe, Takashi, Inatani, Yoshifumi

Publikováno v: 宇宙航行の力学シンポジウム平成15年度 = Symposium on Flight Mechanics and Astrodynamics 2003. :13-16

資料番号: AA0047120004

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::6127b8f4f143db1551ca7f64a62303a3
http://id.nii.ac.jp/1696/00014643/

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Evaluation of shock layer gas temperatures in USERS/READ experiment

Autor: Fujita, Kazuhisa, Abe, Takashi, Wakabayashi, Akira, Ijichi, Koichi

Publikováno v: 宇宙航行の力学シンポジウム平成15年度 = Symposium on Flight Mechanics and Astrodynamics 2003. :5-8

In order to obtain the thermochemical information about the reentry environments around the reentry vehicle, the reentry environment advanced diagnostics (READ) experiment was performed onboard the USERS reentry vehicle during the reentry from the lo

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::8764d20d5185e9a5703f60900702933f
http://id.nii.ac.jp/1696/00014641/

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An induction heater for simulating the environment at planetary atmosphere entry

Autor: Yamada, Tetsuya, Suzuki, Naohiro, Inatani, Yoshifumi

Publikováno v: 宇宙航行の力学シンポジウム平成15年度 = Symposium on Flight Mechanics and Astrodynamics 2003. :111-114

大気をもつ惑星・衛星への探査プローブ投入など、将来の惑星突入ミッションに対応して突入カプセルの耐熱材料の地上試験を行うためには、地上にて突入飛行環境を模擬した高エンタ�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::4011db900f35bdd0c17aaf611e7cf6ef
http://id.nii.ac.jp/1696/00014668/

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Reconstruction of the reentry flight environment based on USERS capsule flight data

Autor: Yamada, Tetsuya, Ishii, Nobuaki, Matsuda, Seiji

Publikováno v: 宇宙航行の力学シンポジウム平成15年度 = Symposium on Flight Mechanics and Astrodynamics 2003. :1-4

USERSカプセルは軌道上の実験後、地球周回軌道からの再突入を行い回収された、国産技術により開発された初のカプセルである。ここでは、その再突入飛行、再突入飛行環境計測実験(READ

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::ca9a6a8c5f874f6a40f9dad916e4c586
http://id.nii.ac.jp/1696/00014640/

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Application of observation data of a hypervelocity reentry capsule to planetary science

Autor: Yano, Hajime, Yamada, Tetsuya, Abe, Shinsuke, Ishihara, Yoshiaki, Yanagisawa, Toshifumi, Fujita, Kazuhisa

Publikováno v: 宇宙航行の力学シンポジウム平成15年度 = Symposium on Flight Mechanics and Astrodynamics 2003. :9-12

資料番号: AA0047120003

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::c293617df1dacb6a7d95bdc4fc517a91
http://id.nii.ac.jp/1696/00014642/

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Marco Polo capsule and DASH-2 plan

Autor: Yamada, Tetsuya, Yoshikawa, Makoto, Kawaguchi, Junichiro

Publikováno v: 第29回太陽系科学シンポジウム平成19年度 = 29th Solar System Exploration Symposium 2007. :72-74

資料番号: AA0063719017

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::422e7b70e6d565edab3a8b4abd7978c2
http://id.nii.ac.jp/1696/00019954/

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Stabilization time of the flow field around spacecraft in an experiment using a shock tunnel

Autor: Nishio, Masatomi, Manabe, Keiji, Sezaki, Shinji, Nakamura, Hiroaki

Publikováno v: 宇宙航行の力学シンポジウム平成15年度 = Symposium on Flight Mechanics and Astrodynamics 2003. :29-30

資料番号: AA0047120008

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::e3f0159d8a813b2413339d54e46ba3b0
http://id.nii.ac.jp/1696/00014647/

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