Ignition transient model for large aspect ratio sole) rocket motors

32nd Joint Propulsion Conference and Exhibit

Volumn , Issue , 1996, Pages

  Luke, G D ^a   Eagar, M A ^b   Dwyer, H A ^c  

^a AEROJET ROCKETDYNE   (United States)

^b Chemical Systems Division   (United States)

^c UNIVERSITY OF CALIFORNIA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ASPECT RATIO; CODES (SYMBOLS); FLAME RESEARCH; FORECASTING; HEAT TRANSFER; PROPULSION; ROCKET ENGINES; ROCKETS; SPACE SHUTTLES;

COMPUTER MODELING; FLAME SPREAD RATE; IGNITION TRANSIENT; LARGE ASPECT RATIO; NUMERICAL COMPLEXITY; PROPELLANT GRAIN; SOLID ROCKET MOTORS; START CHARACTERISTICS;

RELUCTANCE MOTORS;

EID: 84961898804     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (21)

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