Development and flight test of metal-lined CFRP cryogenic tank for reusable rocket

Author:

Higuchi Ken,Takeuchi Shinsuke,Sato Eiichi,Naruo Yoshihiro,Inatani Yoshifumi,Namiki Fumiharu,Tanaka Kohtaro,Watabe Yoko

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference4 articles.

1. Concept and preliminary flight testing of a fully reusable rocket vehicle;Inatani;Journal of Spacecraft and Rockets,2001

2. H. Yamakawa, K. Higuchi, T. Maruyama, N. Kubota, Flight evaluation of GN&C system and vertical landing dynamics of reusable rocket vehicle, AIAA-2001-1907, in: Proceedings of the 10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference, Kyoto, Japan, 24–27 April 2001.

3. N. Takeda, T. Mizutani, Real-time strain measurement of a composite LH2 tank mounted on a reusable rocket test vehicle using an onboard FBG measurement system, in: Proceedings of the Second European Conference on Structural Health Monitoring, Munich/Germany, 7–9 July 2004.

4. Y. Inatani, Y. Naruo, N. Ishii, H. Ogawa, S. Nonaka, H. Yamakawa, Recent progress in reusable rocket vehicle testing campaign, in: Proceedings of the 24th International Symposium on Space Technology and Science, Miyazaki, Japan, 1–6 June 2004.

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