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Dynamic testing for shuttle design verificationSpace shuttle design verification requires dynamic data from full scale structural component and assembly tests. Wind tunnel and other scaled model tests are also required early in the development program to support the analytical models used in design verification. Presented is a design philosophy based on mathematical modeling of the structural system strongly supported by a comprehensive test program; some of the types of required tests are outlined.
Document ID
19720023225
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Green, C. E. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Leadbetter, S. A. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Rheinfurth, M. H. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 6, 2013
Publication Date
July 1, 1972
Publication Information
Publication: NASA Space Shuttle Technol. Conf.
Subject Category
Space Vehicles
Accession Number
72N30875
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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IDRelationTitle19720023215Collected WorksNASA Space Shuttle Technology Conference: Dynamics and Aeroelasticity; Structures and MaterialsN72-30865 21-31Collected Works
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