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Space shuttle plume/simulation applicationAn analysis of pressure and strain-gage data from space shuttle wind tunnel test IA119 and IA138 was performed to define the influence on aerodynamic characteristics resulting from the main propulsion system and solid rocket booster plumes. Aerodynamic characteristics of each of the elements, the components and total vehicle of the space shuttle vehicle during ascent flight was considered. Pressure data were obtained over the aft portions of the space shuttle wind tunnel model in addition to wing and elevon gage data.
Document ID
19790021050
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Boyle, W. (Northrop Services, Inc. Huntsville, AL, United States)
Conine, B. (Northrop Services, Inc. Huntsville, AL, United States)
Bell, G. (Northrop Services, Inc. Huntsville, AL, United States)
Date Acquired
September 3, 2013
Publication Date
May 15, 1979
Subject Category
Space Transportation
Report/Patent Number
TR-230-1964
NASA-CR-161275
Report Number: TR-230-1964
Report Number: NASA-CR-161275
Accession Number
79N29221
Funding Number(s)
CONTRACT_GRANT: NAS8-32524
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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