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Experimental and theoretical analysis of ablative material response in a liquid- propellant rocket engine Final reportAblative material degradation in liquid propellant rocket engine environment of nitrogen tetroxide-aerozine
Document ID
19680000563
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Clark, K. J. (Aerotherm Corp. Palo Alto, CA, United States)
Flood, D. T. (Aerotherm Corp. Palo Alto, CA, United States)
Moyer, C. B. (Aerotherm Corp. Palo Alto, CA, United States)
Rindal, R. A. (Aerotherm Corp. Palo Alto, CA, United States)
Date Acquired
August 4, 2013
Publication Date
September 1, 1967
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-CR-72301
REPT.-67-15
Report Number: NASA-CR-72301
Report Number: REPT.-67-15
Accession Number
68N10031
Funding Number(s)
CONTRACT_GRANT: NAS3-7945
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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