Multidisciplinary Analysis and Optimisation approach for the design of expendable launchers

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

Volumn 3, Issue , 2004, Pages 1597-1611

  Duranté, Nicolas ^a,c   Dufour, Alain ^a,d   Pain, Véronique ^a,e   Baudrillard, Gilles ^a,f   Schoenauer, Marc ^b,g  

^a AIRBUS GROUP INNOVATIONS   (Germany)

^b INRIA   (France)

^c Mission Analysis Section   (France)

^d Propulsion Department

^e Mission Analysis and Guidance Department

^f Engineering and Information Technologies Department

^g UFR 919 Laboratoire d'Informatique Pour la Mécanique et les Sciences de l'Ingénieur   (France)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; CONSTRAINT THEORY; FLIGHT DYNAMICS; LOADING; OPTIMIZATION; PARAMETER ESTIMATION; PROBLEM SOLVING; SPACECRAFT PROPULSION;

EXPENDABLE LAUNCHERS; OPTIMIZATION APPROACH; PAYLOADS; SINGLE PROCESS;

CATAPULTS (AIRCRAFT LAUNCHERS);

EID: 20344394915     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-4441     Document Type: Conference Paper

References (3)

1. T. Bäck. Evolutionary Algorithms in Theory and Practice. New-York Oxford University Press, 1995
2. th International Astronautical Congress.
3. th Int. Conf. on Launcher Technology, Liquid Propulsion.