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Volumn , Issue , 1997, Pages
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Ignition and unsteady combustion of ap-based composite propellants in subscale solid rocket motors with nozzle seal
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Author keywords
[No Author keywords available]
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Indexed keywords
ATMOSPHERIC TEMPERATURE;
COMBUSTION;
COMPUTATIONAL FLUID DYNAMICS;
HEAT CONDUCTION;
HEAT FLUX;
IGNITION;
ONE DIMENSIONAL;
PROPELLANTS;
PROPULSION;
ROCKET ENGINES;
ROCKET NOZZLES;
ROCKETS;
TURBULENCE MODELS;
ANALYTICAL DESCRIPTION;
ANALYTICAL PROCEDURE;
COMPUTATION PROCESS;
IGNITION PROPAGATION;
PROPELLANT BURNING RATE;
STEADY-STATE EXPRESSION;
SURFACE TEMPERATURES;
UNSTEADY HEAT CONDUCTION;
COMPOSITE PROPELLANTS;
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EID: 84962788127
PISSN: None
EISSN: None
Source Type: Conference Proceeding
DOI: None Document Type: Conference Paper |
Times cited : (1)
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References (11)
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