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Managing Uncertainty in Preliminary Aeroshell Design AnalysisAn analysis tool to aid in preliminary design of re-entry aeroshells for interplanetary exploration is presented. The computational tool addresses a common feature of design analysis, the need to make use of results from several analysis regimes and from several sources.
Document ID
20060035408
Acquisition Source
Jet Propulsion Laboratory
Document Type
Preprint (Draft being sent to journal)
External Source(s)
hdl:2014/22413
Authors
Scott, M. J.
kaiser, R. W.
Dilligan, M.
Glaser, R. J.
Antonsson, E. K.
Date Acquired
August 23, 2013
Publication Date
September 14, 1997
Distribution Limits
Public
Copyright
Other
Keywords
Design Methods and Models Design Representations Computational Methods of Design

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