Heat flux and internal ballistic characterization of a hybrid rocket motor analog

33rd Joint Propulsion Conference and Exhibit

Volumn , Issue , 1997, Pages

  Chiaverini, Martin J ^a   Kuo, Kenneth K ^a   Peretz, Arie ^a   Harting, George C ^a  

^a The Center for Nanotechnology Education and Utilization   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ALUMINUM; BOUNDARY LAYER FLOW; BOUNDARY LAYERS; CARBON DIOXIDE; COMBUSTION; FUELS; GASES; HEAT CONVECTION; NUMERICAL METHODS; PROPULSION; PYROLYSIS; RADIANT HEATING; RADIATION EFFECTS; REGRESSION ANALYSIS; ROCKET ENGINES; SHEAR FLOW; SOOT;

GAS-PHASE COMBUSTION; HYBRID ROCKET MOTORS; NON-DIMENSIONAL PARAMETERS; NUMERICAL TECHNIQUES; SEMI-EMPIRICAL METHODS; SOLID FUEL PYROLYSIS; ULTRAFINE ALUMINUM POWDERS; VARIABLE FLUID PROPERTIES;

HEAT FLUX;

EID: 84962832668     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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