Optimal design of hybrid motor for the first stage of air launch vehicle

39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2003, Pages

  Kwon, Sun Tak ^a   Park, Bong Kyo ^a   Lee, Changjin ^a   Lee, Jae Woo ^a  

^a Konkuk University   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

AIR LAUNCH VEHICLE; COMMERCIAL SERVICES; DESIGN VARIABLES; MISSION REQUIREMENTS; NOZZLE EXPANSION RATIO; OPTIMAL DESIGN; PHYSICAL CONSTRAINTS; VEHICLE DESIGN;

COMBUSTION CHAMBERS; COMMERCIAL VEHICLES; DESIGN; NANOSATELLITES; OPTIMAL SYSTEMS; OPTIMIZATION; PROPULSION; ROCKETS;

LAUNCH VEHICLES;

EID: 84897585897     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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