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Results of dynamic stability tests conducted on a .012 scale model modified 089 B shuttle orbiter in the AEDC-VKF tunnel B at a Mach number of 8.0 (LA42)Experimental aerodynamic investigations were conducted on a .012 scale model of a NASA/Langley modified version of the Rockwell 089B Space Shuttle Orbiter. Using the forced oscillation test technique, dynamic stability derivatives were measured in the pitch, yaw and roll planes at a Mach number of 8 over an angle of attack range from -4 deg to 28 deg. Plotted and tabulated results are presented.
Document ID
19750016745
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Vaughn, J. E. (Chrysler Corp. New Orleans, LA, United States)
Daviet, J. T. (Chrysler Corp. New Orleans, LA, United States)
Date Acquired
September 3, 2013
Publication Date
May 1, 1975
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
DMS-DR-2132
NASA-CR-141535
Accession Number
75N24817
Funding Number(s)
CONTRACT_GRANT: NAS9-13247
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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