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Supersonic dynamic stability derivatives of a modified 089B shuttle orbiterAn experimental test program was conducted to measure the dynamic stability derivatives of a modified 089B shuttle orbiter. Supersonic forced oscillation tests were conducted in the Langley Unitary Plan Wind Tunnel over a range of Mach numbers from 1.6 to 4.63 for angles of attack up to 30 deg. The data were measured at the model resonant frequency with pitch and yaw amplitudes of 1 deg and a roll amplitude of 2.5 deg.
Document ID
19750006740
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Freeman, D. C. (NASA Langley Research Center Hampton, VA, United States)
Boyden, R. P. (NASA Langley Research Center Hampton, VA, United States)
Davenport, E. E. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
October 1, 1974
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-TM-X-72630
Report Number: NASA-TM-X-72630
Accession Number
75N14812
Funding Number(s)
CONTRACT_GRANT: NAS9-13247
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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