This paper presents a probabilistic optimization methodology for aerospace vehicle design under uncertainty. The inclusion of linkages between system-level and component-level design requirements leads to multidisciplinary optimization (MDO). The proposed methodology formulates and solves a probabilistic multidisciplinary optimization problem for the coupled design of a reusable launch vehicle (RLV) geometry and its liquid hydrogen fuel tank.
Aerospace Vehicle Conceptual Design under Uncertainty
Ninth Biennial Conference on Engineering, Construction, and Operations in Challenging Environments ; 2004 ; League City, Houston, Texas, United States
2004-03-03
Conference paper
Electronic Resource
English
Aerospace Vehicle Conceptual Design under Uncertainty
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