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Orbiter/shuttle carrier aircraft separation: Wind tunnel, simulation, and flight test overview and resultsA summary of the approach and landing test phase of the space shuttle program is given from the orbiter/shuttle carrier aircraft separation point of view. The data and analyses used during the wind tunnel testing, simulation, and flight test phases in preparation for the orbiter approach and landing tests are reported.
Document ID
19800016876
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Homan, D. J.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Denison, D. E.
(Rockwell International Corp. Downey, Calif., United States)
Elchert, K. C.
(Rockwell International Corp. Downey, Calif., United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1980
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-TM-58223
Report Number: NASA-TM-58223
Accession Number
80N25372
Funding Number(s)
PROJECT: RTOP 953-36-00-00-72
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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