Burning Rate Augmentation of BAMO Based Propellants

Author:

Oyumi Yoshio,Inokami Kiyotaka,Yamazaki Kazuhiro,Matsumoto Koki

Publisher

Wiley

Subject

General Chemical Engineering,General Chemistry

Reference12 articles.

1. and ?HMX Combustion Modification?, Final Report to Air Force Rocket Propulsion Lab., AFRPL-TR-84-044, AD-A145071 (1984).

2. ?Critical Analysis of Nitramine Decomposition Data: Product Distributions from HMX and RDX Decomposition?, Technical Report to US Army Ballsitic Research Lab., BRL-TR-2659, AD-A159325 (1985).

3. ?Studies of the Effect of Hivelite and Other Boron Compounds on Nitramine Decomposition by pyrolysis GC-FTIR?, Technical Report to US Army Ballistic Research Lab., BRL-TR-2973, AD-A206802 (1988).

4. ?Borohydride Catalysis of Nitramine Thermal Decomposition and Combustion. II. Thermal Decomposition of Catalyzed and Uncatalyzed HMX Propellant Formulations?, Technical Report to US Army Ballistic Research Lab., BRL-TR-3078, AD-A220303 (1990).

5. Thermal decomposition of energetic materials 12. Infrared spectral and rapid thermolysis studies of azide-containing monomers and polymers

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