Supersonic and Subsonic Wind Tunnel Heat-Transfer Measurements in the Base Cavity Region of the Shuttle Solid Rocket Booster During Simulated Reentry

Supersonic and Subsonic Wind Tunnel Heat-Transfer Measurements in the Base Cavity Region of the Shuttle Solid Rocket Booster During Simulated Reentry
Author: W. R. Hawkins
Publisher:
Total Pages: 42
Release: 1982
Genre:
ISBN:

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Tests were conducted on the aft section of the Space Shuttle Solid Rocket Booster at Mach numbers 3.75 and 0.5 at selected angles of attack from 90-180 deg simulating reentry attitudes. The tests wre conducted in the AEDC Supersonic Wind Tunnel A to obtain heat-transfer coefficients in the base cavity region. (Author).

Report

Report
Author: United States. National Bureau of Standards
Publisher:
Total Pages: 232
Release: 1956
Genre: Hydraulic engineering
ISBN:

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NBS Special Publication

NBS Special Publication
Author:
Publisher:
Total Pages: 226
Release: 1918
Genre: Weights and measures
ISBN:

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