Combustion mechanism of RDX and HMX and possibilities of controlling the combustion characteristics of systems based on them

Combustion, Explosion and Shock Waves

Volumn 49, Issue 1, 2013, Pages 53-63

  Strunin, V A ^a   Nikolaeva, L I ^a  

^a INSTITUTE OF PROBLEMS OF CHEMICAL PHYSICS   (Russian Federation)

Author keywords

Combustion mechanism; Control of combustion characteristics; HMX; Modeling; RDX; Solid rocket propellant

Indexed keywords

AMMONIUM PERCHLORATES; BINARY COMPOSITION; CHARACTERISTIC PARTICLES; CHEMICAL INTERACTIONS; COMBUSTION CHARACTERISTICS; COMBUSTION MECHANISM; CONDENSED PHASE; CYCLIC NITRAMINES; GAS PHASIS; HEAT EXCHANGE; HIGH PRESSURE; JOINT EFFECT; LOW PRESSURES; PURE SUBSTANCES; RDX; SOLID ROCKET PROPELLANT; TERNARY COMPOSITION;

HMX; MODELS; SOLID PROPELLANTS;

COMBUSTION;

EID: 84873343696     PISSN: 00105082     EISSN: 15738345     Source Type: Journal    
DOI: 10.1134/S0010508213010061     Document Type: Article

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