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Solid rocket motor witness testThe Solid Rocket Motor Witness Test was undertaken to examine the potential for using thermal infrared imagery as a tool for monitoring static tests of solid rocket motors. The project consisted of several parts: data acquisition, data analysis, and interpretation. For data acquisition, thermal infrared data were obtained of the DM-9 test of the Space Shuttle Solid Rocket Motor on December 23, 1987, at Thiokol, Inc. test facility near Brigham City, Utah. The data analysis portion consisted of processing the video tapes of the test to produce values of temperature at representative test points on the rocket motor surface as the motor cooled down following the test. Interpretation included formulation of a numerical model and evaluation of some of the conditions of the motor which could be extracted from the data. These parameters included estimates of the insulation remaining following the tests and the thickness of the charred layer of insulation at the end of the test. Also visible was a temperature signature of the star grain pattern in the forward motor segment.
Document ID
19920004055
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Welch, Christopher S.
(College of William and Mary Williamsburg, VA, United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1991
Publication Information
Publisher: NASA
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NAS 1.26:4415
NASA-CR-4415
Report Number: NAS 1.26:4415
Report Number: NASA-CR-4415
Accession Number
92N13273
Funding Number(s)
PROJECT: RTOP 505-63-01-17
CONTRACT_GRANT: NAS1-18347
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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