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Predicted and flight test results of the performance, stability and control of the space shuttle from reentry to landingAerodynaic performance, stability and control data obtained from the first five reentries of the Space Shuttle orbiter are given. Flight results are compared to pedicted data from Mach 26.4 to Mach 0.4. Differences between flight and predicted data as well as probable causes for the discrepancies are given.
Document ID
19840002069
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kirsten, P. W. (Air Force Flight Test Center Edwards AFB, CA, United States)
Richardson, D. F. (Air Force Flight Test Center Edwards AFB, CA, United States)
Wilson, C. M. (Air Force Flight Test Center Edwards AFB, CA, United States)
Date Acquired
August 12, 2013
Publication Date
October 1, 1983
Publication Information
Publication: NASA. Langley Research Center Shuttle Performance: Lessons Learned, Pt. 1
Subject Category
Space Transportation
Accession Number
84N10136
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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IDRelationTitle19840002048Collected WorksShuttle Performance: Lessons Learned, part 1
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