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Structural tailoring of SSME turbopump blades (SSME/STAEBL)Computer structural optimization is applied to the design of Space Shuttle main engine turbopump blades. The optimization is implemented by the program SSME/STAEBL. A general description of this program is given. Design optimization studies for typical blade designs are presented.
Document ID
19860054157
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rubinstein, R. (Sverdrup Technology, Inc. Middleburg Heights, OH, United States)
Chamis, C. C. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1986
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 86-0847
Accession Number
86A38895
Distribution Limits
Public
Copyright
Other

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