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Probabilistic Sensitivity Analysis for Launch Vehicles with Varying Payloads and Adapters for Structural Dynamics and LoadsThis paper examines Probabilistic Sensitivity Analysis (PSA) methods and tools in an effort to understand their utility in vehicle loads and dynamic analysis. Specifically, this study addresses how these methods may be used to establish limits on payload mass and cg location and requirements on adaptor stiffnesses while maintaining vehicle loads and frequencies within established bounds. To this end, PSA methods and tools are applied to a realistic, but manageable, integrated launch vehicle analysis where payload and payload adaptor parameters are modeled as random variables. This analysis is used to study both Regional Response PSA (RRPSA) and Global Response PSA (GRPSA) methods, with a primary focus on sampling based techniques. For contrast, some MPP based approaches are also examined.
Document ID
20120014367
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
McGhee, David S.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Peck, Jeff A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
McDonald, Emmett J.
(Jacobs Technologies Engineering Science Contract Group Huntsville, AL, United States)
Date Acquired
August 26, 2013
Publication Date
April 23, 2012
Subject Category
Statistics And Probability
Report/Patent Number
M11-0845
Meeting Information
Meeting: 14th AIAA Non-Deterministic Approaches Conference
Location: Honolulu, HI
Country: United States
Start Date: April 23, 2012
End Date: April 26, 2012
Sponsors: American Inst. of Aeronautics and Astronautics, American Society of Civil Engineers, American Helicopter Society, Inc., American Society of Mechanical Engineers, American Society for Composites
Distribution Limits
Public
Copyright
Public Use Permitted.
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