Response surface equations for expendable launch vehicle payload capability

AIAA Space 2009 Conference and Exposition

Volumn , Issue , 2009, Pages

  Fleming, Elizabeth S ^a   Lafleur, Jarret M ^a   Saleh, Joseph H ^a  

^a Georgia Institute of Technology   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERS; CIRCULAR ORBIT; DESIGN AND DEVELOPMENT; EXPENDABLE LAUNCH VEHICLES; FIRST-ORDER; FITTING METHOD; GOODNESS-OF-FIT TEST; LAUNCH VEHICLE; LAUNCH VEHICLE PAYLOADS; MASS GROWTH; MODEL FIT; ORBIT ALTITUDE; ORBIT INCLINATION; ORBIT PERFORMANCE; ORBITAL PARAMETERS; PAYLOAD CAPABILITIES; PEGASUS; RESPONSE SURFACE; SPACECRAFT MASS;

AEROSPACE ENGINEERING; COMMERCE; CONCEPTUAL DESIGN; ENGINEERS; ERROR STATISTICS; LAUNCH VEHICLES; ORBITAL LABORATORIES; ORBITS; STATISTICAL TESTS; SURFACE PROPERTIES; SYSTEMS ANALYSIS; VEHICLES;

LAUNCHING;

EID: 77958585137     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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