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Begell House作者,编辑及审稿者

Keiichi Hori

Institute of Space and Astronautical Science (ISAS), Japan Aerospace Exploration Agency (JAXA), 3-1-1 Yoshinodai, Chuo-Ku, Sagamihara, Kanagawa 252-5210, Japan

Journals

Articles

GLYCIDYL AZIDE POLYMER AND POLYETHYLENE GLYCOL MIXTURES AS HYBRID ROCKET FUELS Vol. 11 '2012 - International Journal of Energetic Materials and Chemical Propulsion
GLYCIDYL AZIDE POLYMER−COMBUSTION MECHANISM AND ITS APPLICATION TO HYBRID ROCKET MOTORS Vol. 11 '2012 - International Journal of Energetic Materials and Chemical Propulsion
A STUDY ON THE COMBUSTION MECHANISM OF HYDROXYLAMMONIUM NITRATE Vol. 14 '2015 - International Journal of Energetic Materials and Chemical Propulsion
COMBUSTION AND PERFORMANCE STUDIES OF GLYCIDYL AZIDE POLYMER AND ITS MIXTURES AS HYBRID ROCKET FUEL Vol. 14 '2015 - International Journal of Energetic Materials and Chemical Propulsion
OBSERVATION OF COMBUSTION BEHAVIOR OF LOW MELTING TEMPERATURE FUEL FOR A HYBRID ROCKET USING DOUBLE SLAB MOTOR Vol. 15 '2016 - International Journal of Energetic Materials and Chemical Propulsion
ADVANCED ENERGETIC MATERIALS AND TECHNIQUES FOR ROCKET PROPULSION: IN HONOR OF PROF. KENNETH KUAN-YUN KUO Vol. 16 '2017 - International Journal of Energetic Materials and Chemical Propulsion
ADVANCED ENERGETIC MATERIALS AND TECHNIQUES FOR ROCKET PROPULSION: IN HONOR OF PROF. KENNETH KUAN-YUN KUO Vol. 16 '2017 - International Journal of Energetic Materials and Chemical Propulsion
PREFACE: "ADVANCED ENERGETIC MATERIALS AND TECHNIQUES FOR ROCKET PROPULSION" IN HONOR OF PROF. KENNETH KUAN-YUN KUO Vol. 16 '2017 - International Journal of Energetic Materials and Chemical Propulsion
DEVELOPMENT OF A DIRECT INJECTION GAS-HYBRID ROCKET SYSTEM USING GLYCIDYL AZIDE POLYMER Vol. 18 '2019 - International Journal of Energetic Materials and Chemical Propulsion
IMPROVEMENT OF COMBUSTION EFFICIENCY USING A BAFFLE PLATE FOR A LT/GOX HYBRID ROCKET MOTOR Vol. 18 '2019 - International Journal of Energetic Materials and Chemical Propulsion
PYROLYSIS BEHAVIOR OF A PARAFFIN-BASED THERMOPLASTIC POLYMER USED IN HYBRID ROCKET FUEL Vol. 18 '2019 - International Journal of Energetic Materials and Chemical Propulsion
PREFACE: OBITUARY FOR DR. ARIE PERETZ Vol. 19 '2020 - International Journal of Energetic Materials and Chemical Propulsion
BURNING RATE AND PRESSURE DEFLAGRATION LIMIT (PDL) CHARACTERISTICS OF A GAP/AP PROPELLANT SYSTEM Vol. 5 '2002 - International Journal of Energetic Materials and Chemical Propulsion
MODIFIED BURNING RATE SPECTRUM & COMBUSTION MECHANISM OFTETRA-OLGAP Vol. 6 '2007 - International Journal of Energetic Materials and Chemical Propulsion
COMBUSTION CHARACTERISTICS OF HAN-BASED LIQUID MONOPROPELLANT Vol. 7 '2008 - International Journal of Energetic Materials and Chemical Propulsion
DEVELOPMENT OF HAN-BASED LIQUID PROPELLANT THRUSTER Vol. 7 '2008 - International Journal of Energetic Materials and Chemical Propulsion
BASIC STUDY OF GAS GENERANT IN AIR BAG INFLATORS Vol. 8 '2009 - International Journal of Energetic Materials and Chemical Propulsion
COMBUSTION MECHANISM OF TETRA-OL GLYCIDYL AZIDE POLYMER AND ITS APPLICATION TO HYBRID ROCKETS Vol. 8 '2009 - International Journal of Energetic Materials and Chemical Propulsion
MICRO SOLID PROPELLANT THRUSTER FOR SMALL SATELLITE Vol. 8 '2009 - International Journal of Energetic Materials and Chemical Propulsion
COMBUSTION CHARACTERISTICS OF HYDROXYLAMMONIUM NITRATE AQUEOUS SOLUTIONS Vol. 9 '2010 - International Journal of Energetic Materials and Chemical Propulsion
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