An automated approach to multidisciplinary system design optimization of small solid propellant launch vehicles

1st International Symposium on Systems and Control in Aerospace and Astronautics

Volumn 2006, Issue , 2006, Pages 1401-1406

  Jodei, Jahangir ^a   Ebrahimi, Masoud ^a   Roshanian, Jafar ^a  

^a K N TOOSI UNIVERSITY OF TECHNOLOGY   (Iran)

Author keywords

[No Author keywords available]

Indexed keywords

AUTOMATED DESIGN OPTIMIZATION; QUADRATIC RESPONSE SURFACE EQUATIONS; RESPONSE SURFACE APPROXIMATION; SMALL SOLID PROPELLANT LAUNCH VEHICLES;

APPROXIMATION THEORY; AUTOMATION; MACHINE DESIGN; MATHEMATICAL MODELS; OPTIMIZATION; SPACECRAFT PROPULSION;

CATAPULTS (AIRCRAFT LAUNCHERS);

EID: 33750945164     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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