1–20 of 47 hits
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    Combustion Characteristics of Gas Hybrid Rocket using H~2O/HNO~3 as Oxidizer (AIAA 2015-4136)

    Suzuki, Ikki / Kuwahara, Takuo | British Library Conference Proceedings | 2015

    Combustion characteristic of solid propellants used H2O

    Sasaki, Takafumi / Takahashi, Kenichi / Kuwahara, Takuo | AIAA | 2015

    Characteristics of aluminum agglomeration at burning surface in AP/AN composite propellants

    Oide, Sho / Takahashi, Kenichi / Kuwahara, Takuo | AIAA | 2012

    Combustion Characteristic of Solid Propellants Used H2O (AIAA 2015-0926)

    Sasaki, Takafumi / Takahashi, Kenichi / Kuwahara, Takuo | British Library Conference Proceedings | 2015

    Effect of Pressure on Decomposition and Ignition of GAP Single Droplet

    Tamura, Goichi / Tanabe, Mituaki / Kuwahara, Takuo | AIAA | 2011

    Surface Temperature of Agglomerated Aluminum Particles in a Reaction Zone

    Doi, Rieko / Kuwahara, Takuo / Yamamoto, Kengo et al. | AIAA | 2017

    Ignition characteristics of Zr/BaCrO4 pyrolant

    Kuwahara, Takuo / Tohara, Chiharu | Tema Archive | 2002

    Ignition Characteristics of Boron Particles in Ducted Rockets

    Odawara, Takaki / Tanabe, Mitsuaki / Kuwahara, Takuo | AIAA | 2005

    Combustion Characteristics of Boron Particles in The Secondary Combustor of Ducted Rockets

    Kazaoka, Yuji / Takahashi, Kenichi / Tanabe, Mituaki et al. | AIAA | 2011

    Ignition Characteristics of Zr with Micro Ducted Rockets

    Oshima, Hideto / Tanabe, Mitsuaki / Kuwahara, Takuo | AIAA | 2006

    Development of a Micro Thruster with Large Thrust

    Otomo, Kenji / Tanabe, Mitsuaki / Kuwahara, Takuo | AIAA | 2008