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Fatigue loads spectra derivation for the Space Shuttle: Second cycleSome of the environments and loads experienced by the Space Shuttle or future reusable space vehicles are unique, while others are similar to those encountered by commercial and/or military aircraft. Prior to the Space Transportation System (STS) flights, fatigue loads spectra were generated for the Space Shuttle based on anticipated environments and assumptions that were shown not to be applicable to the actual flight environments the vehicle experienced. This resulted in the need to generate a new cycle of fatigue loads spectra, which was based on measured flight data as well as mission profiles, reflecting the various types of service and operations the vehicle and payloads experienced.
Document ID
19950013054
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
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 Tolerane, Part 2
Subject Category
Structural Mechanics
Accession Number
95N19470
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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