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Reactivation and upgrade of the NASA Ames 16-Inch Shock Tunnel - Status reportThe NASA Ames 16-Inch Shock Tunnel has been reactivated after seventeen years of inactivity. In the years before deactivating the facility, it was operated at enthalpies of 4,700 J/gm and pressures up to 260 atm or at enthalpies of 1900 J/gm over a wide pressure range. Since reactivating, the facility has been operated at enthalpies up to 12,000 J/gm and pressures up to 408 atm. The present paper describes the steps taken in upgrading the facility and summarizes the currently achievable conditions. The selection of the driver gas, the steps taken to improve the driver burn, and the diaphragm opening techniques are described. The pressure and heat flux instrumentation, the optical diagnostics and the data acquisition system are also described.
Document ID
19920043150
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bogdanoff, David W.
(NASA Ames Research Center Moffett Field, CA, United States)
Zambrana, Horacio A.
(Eloret Institute Palo Alto, CA, United States)
Cavolowsky, John A.
(NASA Ames Research Center Moffett Field, CA, United States)
Newfield, Mark E.
(NASA Ames Research Center Moffett Field, CA, United States)
Cornelison, Charles J.
(NASA Ames Research Center Moffett Field, CA, United States)
Miller, Robert J.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1992
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
AIAA PAPER 92-0327
Accession Number
92A25774
Funding Number(s)
CONTRACT_GRANT: NCC2-487
Distribution Limits
Public
Copyright
Other

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