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Space Shuttle fatigue loads spectra for prelaunch and liftoff loadsFatigue loads spectra for the prelaunch and liftoff flight segments of the Space Shuttle were developed. A variety o methods were used to determine the distributions of several important parameters, such as time of exposure on the launch, pad, month of launch, and wind speed. Also, some lessons learned that would be applicable to development of fatigue loads spectra for other reusable space vehicles are presented.
Document ID
19950008060
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Goldish, Judith (Rockwell International Corp. Downey, CA, United States)
Ortasse, Raphael (Rockwell International Corp. Downey, CA, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1994
Publication Information
Publication: NASA. Langley Research Center, FAA(NASA International Symposium on Advanced Structural Integrity Methods for Airframe Durability and Damage Tolerance
Subject Category
Space Transportation
Accession Number
95N14474
Funding Number(s)
CONTRACT_GRANT: NAS9-18500
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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