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A review of Space Shuttle payload-bay lift-off flight data and analysis comparisonsThe design evolution of Space Shuttle payloads to be launched requires structural analyses and testing, based on Shuttle load environments, to ensure flight safety and mission success. The adequacy of predicted load environments is continually assessed against flight and ground measured data. The Space Shuttle program has utilized extensive flight measurements to assess payload bay environments. As part of the orbital flight test program on STS-1 through STS-5, the orbiter Columbia was equipped with a broad range of instrumentation, including accelerometers and microphone in the payload bay. The orbiter Challenger was equipped with payload bay measurement systems on six of its flights, and the orbiter Discovery was similarly instrumented beginning with STS-26. The payload bay data, along with other measurements recorded on these flights, are compared to design load requirements for payloads, and updates are made as necessary.
Document ID
19920014553
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hamilton, David A.
(Lockheed Corp. Houston, TX., United States)
Tengler, Nancy E.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Nguyen, B. N.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Lauritzen, Carl A.
(Lockheed Electronics Co. Houston, TX., United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1991
Publication Information
Publication: ESA, Spacecraft Structures and Mechanical Testing, Volume 1
Subject Category
Space Transportation
Accession Number
92N23796
Distribution Limits
Public
Copyright
Other
Document Inquiry

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