Autoren, Herausgeber und Rezensenten von Begell House

A B C D E F G H I J K L M N O P Q R S T U V W X Y Z

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:

International Journal of Energetic Materials and Chemical Propulsion

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

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

Weitere Infos über den Autor erhalten Sie im Expertenverzeichnis