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A tube wind-tunnel technique for rocket propulsion testingShort duration tube wind tunnel supersonic testing, noting Saturn S-1C base heating and solid propellant rocket base burning tests
Document ID
19700063582
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Hendershot, K. C.
Sheeran, W. J.
Date Acquired
August 5, 2013
Publication Date
August 1, 1970
Subject Category
Facilities, Research, And Support
Meeting Information
Meeting: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, AERODYNAMIC TESTING CONFERENCE, 4TH
Location: CINCINNATI, OH
Start Date: April 28, 1969
End Date: April 30, 1969
Sponsors: /AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
70A39698
Funding Number(s)
CONTRACT_GRANT: NAS8-21097
CONTRACT_GRANT: NAS8-20027
Distribution Limits
Public
Copyright
Other

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