1–18 of 18 hits
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    Measurement of shock stand-off distance for sphere in ballistic range

    Nonaka, Satoshi / Takayama, Kazuyoshi / Park, Chul | AIAA | 1997

    Overview of ballistic range program at Tohoku University

    Nonaka, Satoshi / Takayama, Kazuyoshi | AIAA | 1998

    Hypervelocity impact tests with bumper-walled structure against space debris

    Nonaka, Satoshi / Takayama, Kazuyoshi / Kibe, Seishirou | AIAA | 1998

    Ballistic range measurement of shock shapes in intermediate hypersonic regime

    Nonaka, Satoshi / Mizuno, Hiroyasu / Takayama, Kazuyoshi | AIAA | 1999

    Calculation of shock shapes over simple geometry in intermediate hypersonic air flow

    Furudate, Michiko / Nonaka, Satoshi / Sawada, Keisuke | AIAA | 1999

    Behavior of two-temperature model in intermediate hypersonic regime

    Furudate, Michiko / Nonaka, Satoshi / Sawada, Keisuke | AIAA | 1999

    Density measurement over a sphere in ballistic range

    Nonaka, Satoshi / Mizuno, Hiroyasu / Hashimoto, Tokitada et al. | AIAA | 2000

    Aerodynamic design considerations in vertical landing rocket vehicle

    Nonaka, Satoshi / Ogawa, Hiroyuki / Inatani, Yoshifumi | AIAA | 2001

    Microwave Attenuation Measurement of Full-Scale Solid Rocket Motor Plumes

    Funaki, Ikkoh / Ogawa, Hiroyuki / Kato, Teruo et al. | AIAA | 2002

    Prediction of Sloshing in the Propellant Tank of Reusable Rocket Vehicle

    Himeno, Takehiro / Nonaka, Satoshi / Naruo, Yoshihiro et al. | AIAA | 2003

    Thrust Production Mechanism of a Magnetoplasma Sail

    Funaki, Ikkoh / Asahi, Ryusuke / Fujita, Kazuhisa et al. | AIAA | 2003

    A Concept and Its Aerodynamic Design of a Sub-Orbital Reusable Rocket

    Ogawa, Hiroyuki / Nonaka, Satoshi / Inatani, Yoshifumi | AIAA | 2004

    Recent Progress of Reusable Vehicle Testing (RVT) Campaign

    Inatani, Yoshifumi / Naruo, Yoshihiro / Ishii, Nobuaki et al. | AIAA | 2004

    A Concept of a Reusable Sounding Rocket

    Ogawa, Hiroyuki / Naruo, Yoshihiro / Nonaka, Satoshi et al. | AIAA | 2005

    Sloshing Prediction in the Propellant Tanks of VTVL Rocket Vehicle

    Himeno, Takehiro / Watanabe, Toshinori / Nonaka, Satoshi et al. | AIAA | 2005

    Computations of Opposing Jet from Vertical Landing Rocket Vehicle

    Suzuki, Toshiyuki / Nonaka, Satoshi / Inatani, Yoshifumi | AIAA | 2006

    Aerodynamics of Vertical Landing Rocket Vehicle with Engine Thrust in Landing Phase

    Nonaka, Satoshi / Watanabe, Koji / Ogawa, Hiroyuki et al. | AIAA | 2006

    Numerical and Experimental Investigation on Sloshing in Rocket Tanks with Damping Devices

    Himeno, Takehiro / Watanabe, Toshinori / Nonaka, Satoshi et al. | AIAA | 2007