Supersonic and Subsonic Wind Tunnel Heat-Transfer Measurements in the Base Cavity Region of the Shuttle Solid Rocket Booster During Simulated Reentry PDF Download
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Author: W. R. Hawkins
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ISBN:
Category :
Languages : en
Pages : 42
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Book Description
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).
Author: W. R. Hawkins
Publisher:
ISBN:
Category :
Languages : en
Pages : 42
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Book Description
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).
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Category : Heat
Languages : en
Pages : 596
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Category : Science
Languages : en
Pages : 722
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Category :
Languages : en
Pages : 1630
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Category : Aeronautics
Languages : en
Pages : 1280
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Author: Aeronautical Research Council (Great Britain)
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ISBN: 9780114709266
Category : Airplanes
Languages : en
Pages : 1212
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Category : Aeronautics
Languages : en
Pages : 712
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A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA)
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Category :
Languages : en
Pages : 706
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Category : Government reports announcements & index
Languages : en
Pages : 1216
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Category :
Languages : en
Pages : 196
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