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Expanded operational capabilities of the Langley Mach 7 Scramjet test facilityAn experimental research program conducted to expand the operational capabilities of the NASA Langley Mach 7 Scramjet Test Facility is described. Previous scramjet testing in this facility was limited to a single simulated flight condition of Mach 6.9 at an altitude of 115,300 ft. The arc heater research demonstrates the potential of the facility for scramjet testing at simulated flight conditions from Mach 4 (at altitudes from 77,000 to 114,000 ft) to Mach 7 (at latitudes from 108,000 to 149,000 ft). Arc heater electrical characteristics, operational problems, measurements of nitrogen oxide contaminants, and total-temperature profiles are discussed.
Document ID
19830027768
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Thomas, S. R.
(NASA Langley Research Center Hampton, VA, United States)
Guy, R. W.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
October 1, 1983
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NAS 1.60:2186
L-15565
NASA-TP-2186
Report Number: NAS 1.60:2186
Report Number: L-15565
Report Number: NASA-TP-2186
Accession Number
83N36039
Funding Number(s)
PROJECT: RTOP 505-43-83-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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