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An advanced hypervelocity aerophysics facility - A ground-based flight-test rangeThe paper discusses a concept for a ground-based flight-test facility, a large aeroballistic range capable of launching models large enough to permit the installation of significant amounts of onboard instrumentation. The large model size would also provide thick shock/boundary layers, thus providing the opportunity to measure flow-field properties via advanced offboard diagnostics. Current fabrication technology should permit the construction of a two-stage light-gas gun capable of accelerating 20 to 25 cm diameter models to velocities on the order of 6 km/sec. An electromagnetic launcher or a ram accelerator is considered as a potential means for achieving larger model sizes and/or greater launch velocities. Possible methods for obtaining and recording data are discussed as are the test chamber and model deceleration section requirements.
Document ID
19910036822
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Witcofski, R. D.
(NASA Langley Research Center Hampton, VA, United States)
Scallion, W. I.
(NASA Langley Research Center Hampton, VA, United States)
Carter, D. J., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Courter, R. W.
(Louisiana State University Baton Rouge, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1991
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
AIAA PAPER 91-0296
Accession Number
91A21445
Distribution Limits
Public
Copyright
Other

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