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A new arc heater shroud test technique for thermo-structural testing of full-scale, nose-tip skirt materialsAn arc heater shroud test technique was developed for thermostructural testing of full-scale, missile nose tip-skirt assemblies. Reentry trajectory simulation is provided by changing the arc heater operation in a prescribed manner through manual and automatic controls. Excellent test repeatability allows screening of materials by direct comparison of test results. Continuous recordings of model surface temperature, pressure, heat flux, and model internal temperatures are made at several locations during the test.
Document ID
19760004044
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Williams, R. R.
(McDonnell-Douglas Astronautics Co. Saint Louis, MO, United States)
Stultz, J. W.
(McDonnell-Douglas Astronautics Co. Saint Louis, MO, United States)
Popp, R. J.
(McDonnell-Douglas Astronautics Co. Saint Louis, MO, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1975
Publication Information
Publication: NASA. Goddard Space Flight Center. 8th Conf. on Space Simulation
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
PAPER-19
Accession Number
76N11132
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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