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Wind tunnel tests of space shuttle solid rocket booster insulation material in the aerothermal tunnel cWind tunnel tests of the space shuttle Solid Rocket Booster Insulation were conducted in the von Karman Gas Dynamics Facility Tunnel C. For these tests, Tunnel C was run at Mach 4 with a total temperature of 1100-1440 and a total pressure of 100 psia. Cold wall heating rates were changed by varying the test article support wedge angle. Selected results are presented to illustrate the test techniques and typical data obtained.
Document ID
19830011537
Acquisition Source
Legacy CDMS
Document Type
Contractor or Grantee Report
Authors
Hartman, A. S. (Calspan Field Services, Inc. Arnold AFS, TN, United States)
Nutt, K. W. (Calspan Field Services, Inc. Arnold AFS, TN, United States)
Date Acquired
September 4, 2013
Publication Date
November 1, 1982
Publication Information
Publisher: AEDC
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AEDC-TSR-82-V38
Report Number: AEDC-TSR-82-V38
Accession Number
83N19808
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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