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Enhanced capability of the Combustion-Heated Scramjet Test FacilityThe Combustion-Heated Scramjet Test Facility (CHSTF) is described together with its modifications. The expanded simulation capabilities of the facility are documented. Nozzle exit surveys and tunnel calibration information are presented. It is noted that these modifications included a new heat-sink nickel liner heater, a new Mach 4.7 nozzle, and a new 70-ft vacuum sphere exhaust system. It is found that the facility in the air ejector mode of operation performed similarly to that prior to the addition of the vacuum sphere ducting.
Document ID
19910059644
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rock, Kenneth E.
(NASA Langley Research Center Hampton, VA, United States)
Andrews, Earl H.
(NASA Langley Research Center Hampton, VA, United States)
Eggers, James M.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 15, 2013
Publication Date
June 1, 1991
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
AIAA PAPER 91-2502
Accession Number
91A44267
Distribution Limits
Public
Copyright
Other

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