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Direct Visualization of Shock Waves in Supersonic Space Shuttle FlightDirect observation of shock boundaries is rare. This Technical Memorandum describes direct observation of shock waves produced by the space shuttle vehicle during STS-114 and STS-110 in imagery provided by NASA s tracking cameras.
Document ID
20110007108
Acquisition Source
Marshall Space Flight Center
Document Type
Technical Memorandum (TM)
Authors
OFarrell, J. M. (United Space Alliance Huntsville, AL, United States)
Rieckhoff, T. J. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 25, 2013
Publication Date
January 1, 2011
Subject Category
Instrumentation And Photography
Report/Patent Number
M-1304
NASA/TM-2011-216455
Funding Number(s)
CONTRACT_GRANT: NNJ06VA01C
Distribution Limits
Public
Copyright
Public Use Permitted.

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