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Subscale solid motor nozzle tests, phase 4 and nozzle materials screening and thermal characterization, phase 5Subscale solid motor nozzles containing a baseline material or low cost materials to be considered as potential replacements for the baseline material are designed and tested. Data are presented from tests of four identically designed 2.5 inch throat diameter nozzles and one 7 inch throat diameter nozzle. The screening of new candidate low cost materials, as well as their thermophysical and thermochemical characterization is also discussed.
Document ID
19790021055
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Arnold, J.
(Aerotherm Acurex Corp. Mountain View, CA, United States)
Dodson, J.
(Aerotherm Acurex Corp. Mountain View, CA, United States)
Laub, B.
(Aerotherm Acurex Corp. Mountain View, CA, United States)
Date Acquired
September 3, 2013
Publication Date
June 1, 1979
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
TM-79-255
NASA-CR-161254
Report Number: TM-79-255
Report Number: NASA-CR-161254
Accession Number
79N29226
Funding Number(s)
CONTRACT_GRANT: NAS8-30264
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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