Výsledky vyhledávání - "垂直離陸"

Third takeoff/landing experiment of the reusable vehicle test

Autor: Inatani, Yoshifumi

Publikováno v: 宇宙輸送シンポジウム平成15年度 = Proceedings of Space Transportation Symposium FY2003. :190-193

資料番号: AA0047118048

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::0e545b0616d3b4c000762355035c94d1
http://id.nii.ac.jp/1696/00017272/

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Reusable rocket demonstration vehicle system design

Autor: Ogawa, Hiroyuki, Nonaka, Satoshi, Taniguchi, Hirofumi, Aoki, Hiroshi

Publikováno v: 宇宙輸送シンポジウム平成15年度 = Proceedings of Space Transportation Symposium FY2003. :158-161

A baseline configuration of the reusable rocket demonstration vehicle is presented. The vehicle adopts a vertical take-off and vertical landing (VTVL) system to minimize ground support equipments (GSE) and turn-around time. The integrated propulsion

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::1130ea1d03b7fde36e64dabd26832a9b
http://id.nii.ac.jp/1696/00017264/

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レーザー駆動インチューブ加速(LITA)運転におけるレーザーパワー爆破波現象および最適結合係数

Autor: Yu, Xilong, Otani, Toshiro, Watanabe, Keiko, Ogawa, Toshihiro, Saso, Akihiro

Publikováno v: 宇宙輸送シンポジウム平成15年度 = Proceedings of Space Transportation Symposium FY2003. :392-395

The temporal spatial-integrated plasma temperature and blast wave propagation in laser induced blast wave (LSBW) were experimental investigated through emission spectroscopy and shadowgraph system. Experiment results present the detailed wave process

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::0471e30b0fce49859015d5e226c261c9
http://id.nii.ac.jp/1696/00017321/

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Navigation and guidance control in the third takeoff/landing experiment of the reusable vehicle test (RVT)

Autor: Maruyama, Tatsuya, Yamakawa, Hiroshi

Publikováno v: 宇宙輸送シンポジウム平成15年度 = Proceedings of Space Transportation Symposium FY2003. :194-197

資料番号: AA0047118049

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::7997012e67784a48225f89e3e38c425a
http://id.nii.ac.jp/1696/00017273/

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Conceptual design of a two stage reusable rocket

Autor: Iwata, Takumi, Sawada, Keisuke, Kamijo, Kenjiro

Publikováno v: 宇宙航行の力学シンポジウム平成14年度 = Symposium on Flight Mechanics and Astrodynamics 2002. :55-58

資料番号: AA0045913015

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::f34fefcd98963a55176388ea5b9c171e
http://id.nii.ac.jp/1696/00014696/

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Attitude control by the aerodynamic control surface of a vertical takeoff rocket

Autor: Nonaka, Satoshi, Ogawa, Hiroyuki, Osako, Yosuke, Hongo, Motoyuki, Inatani, Yoshifumi

Publikováno v: 宇宙航行の力学シンポジウム平成14年度 = Symposium on Flight Mechanics and Astrodynamics 2002. :51-54

資料番号: AA0045913014

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::a5e17f12e2d028503a1e306c78656ad0
http://id.nii.ac.jp/1696/00014695/

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A study of take-off characteristics of horizontal launch aerospaceplane under ground effect

Autor: Uchida, Norio, Watanabe, Rikio, Tomita, Nobuyuki

Publikováno v: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory. 46:275-280

航空宇宙技術研究所 7-9 Jun. 2000 東京日本
National Aerospace Laboratory 7-9 Jun. 2000 Tokyo Japan
昨今では、垂直打上げ型ロケットが望ましいと考えられているが、将来に亘って宇宙活動のた�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::1a16f57e614dc5e5e92e4d8327e006b4
http://id.nii.ac.jp/1696/00041344/

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再使用型輸送系の研究:離着陸実験構想の検討

Autor: Aoki, Hiroshi, Takano, Yutaka, Ginoza, Akira, Yoshida, Toshiyuki, Iihara, Shigeyasu

Publikováno v: 宇宙開発事業団技術報告 = NASDA Technical Memorandum.

資料番号: AA0010773000
レポート番号: NASDA-TMR-950012T
レポート番号: NASDA-TMR-950012

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::373f0bac7370320642b10b85fd41a1b5
http://id.nii.ac.jp/1696/00041255/

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