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Reentry static stability characteristics of a (Model 471) .005479-scale 146-inch solid rocket booster tested in the NASA/MSFC 14 by 14 inch TWT (SA8F)A force test of a scale model of the Space Shuttle Solid Rocket Booster was conducted in a trisonic wind tunnel. The model was tested with such protuberances as a camera capsule, electrical tunnel, attach rings, aft separation rockets, ET attachment structure, and hold-down struts. The model was also tested with the nozzle at gimbal angles of 0, 2.5, and 5 degrees. The influence of a unique heat shield configuration was also determined. Some photographs of model installations in the tunnel were taken and are included. Schlieren photography was utilized for several angles of attack.
Document ID
19750021090
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Johnson, J. D.
(NASA Marshall Space Flight Center Huntsville, Ala., United States)
Braddock, W. F.
(Northrop Services Inc. Huntsville, Ala., United States)
Praharaj, S. C.
(Northrop Services Inc.)
Date Acquired
September 3, 2013
Publication Date
July 1, 1975
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-CR-141549
DMS-DR-2223
Report Number: NASA-CR-141549
Report Number: DMS-DR-2223
Accession Number
75N29163
Funding Number(s)
CONTRACT_GRANT: NAS9-13247
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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