Weights analysis of space launch vehicles in an advanced engineering environment

Collection of Technical Papers - 10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference

Volumn 5, Issue , 2004, Pages 2893-2901

  Jiang, Xun ^a   Gage, Peter ^a   Vander Kam, Jeremy C ^b,d   Qu, Min ^c,d  

^a ELORET CORPORATION   (United States)

^b NASA AMES RESEARCH CENTER   (United States)

^c Aalytical Mechanics Associates Inc   (United States)

^d ANALYTICAL SERVICES AND MATERIALS INC   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ADVANCED ENGINEERING ENVIRONMENT (AEE); DISPARATE VEHICLES; GROSS LIFT-OFF WEIGHT (GLOW); SPACE LAUNCH VEHICLES;

COMPUTER HARDWARE; COMPUTER SOFTWARE; DATA TRANSFER; MATHEMATICAL MODELS; SOCIETIES AND INSTITUTIONS; SPACECRAFT; XML;

CATAPULTS (AIRCRAFT LAUNCHERS);

EID: 20344392669     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (13)

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13. Lynn, E., "INTROS INTegrated Rocket Sizing Model," User Documentation, Space Transportation Directorate, NASA Marshall Space Flight Center, AL