1–8 von 8 Ergebnissen
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    Detonation engine development for reaction control systems of a spacecraft

    Gawahara, Keita / Nakayama, Hisahiro / Kasahara, Jiro et al. | AIAA | 2013

    Nozuru-resu-roketto-no-kenkyū

    Nakayama, Hisahiro / Daikuhara, Kazuhito / Miyata, Kohsei | TIBKAT | 2005

    A Dual-Mode Scramjet Combustor employing a Jet Fuel for Hypersonic Flight Vehicle

    Nakayama, Hisahiro / Edanaga, Takayuki / Hashino, Seiki et al. | AIAA | 2018

    Front Shock Behavior of Stable Detonation Waves Propagating Through Rectangular Cross-section Curved Channels

    Nakayama, Hisahiro / Moriya, Takahiro / Kasahara, Jiro et al. | AIAA | 2012

    A Dual-Mode Scramjet Combustor Employing a Jet Fuel for Hypersonic Flight Vehicle (AIAA 2018-4452)

    Nakayama, Hisahiro / Edanaga, Takayuki / Hashino, Seiki et al. | British Library Conference Proceedings | 2018

    Performance Demonstration of a Variable Flow Ducted Rocket Engine by Test Flight

    Yamano, Yoshihiro / Ikegami, Yoshiyuki / Nakayama, Hisahiro et al. | AIAA | 2009

    Full-Scale Firing Tests of Variable Flow Ducted Rocket Engines Employing Gap Solid Fuel Gas Generator

    Nakayama, Hisahiro / Ikegami, Yoshiyuki / Yoshida, Akihiko et al. | AIAA | 2009