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Tsuyoshi Oishi, Mitsuru Tamari and Takashi Sakurai
Hybrid rockets are safe and inexpensive; however, boundary-layer combustion poses a problem in achieving a fuel regression rate equivalent to that of solid propellants. The fundamental combustion conditions, such as the fuel regression rate of LT421, a p...
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Tamari, Y. Towhata, I.
Pág. 69 - 88
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Shiraga, H. Azechi, H. Nakai, M. Shigemori, K. Nishikino, M. Sakaiya, T. Fujioka, S. Tamari, Y. Yamanaka, T.
Pág. 2194 - 2197
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Fujioka, S. Shiraga, H. Nishikino, M. Tamari, Y. Shigemori, K. Nakai, M. Azechi, H. Tanaka, K. A. Yamanaka, T.
Pág. 2198 - 2201
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Tamari, Guy; Pappa, Lamprini; Zered, Tamar; Borochov, Amihud
Pág. 29 - 35
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