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Studies of nozzle ablative material performance for large solid boosters Final reportCarbon phenolic, graphite phenolic, and silica phenolic nozzle ablative materials performance for large solid propellant rocket boosters
Document ID
19670005828
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Dahm, T. J. (Aerotherm Corp. Palo Alto, CA, United States)
Schaefer, J. W. (Aerotherm Corp. Palo Alto, CA, United States)
Date Acquired
August 3, 2013
Publication Date
December 15, 1966
Subject Category
Propulsion Systems
Report/Patent Number
REPT.-66-2
NASA-CR-72080
Report Number: REPT.-66-2
Report Number: NASA-CR-72080
Accession Number
67N15157
Funding Number(s)
CONTRACT_GRANT: NAS7-405
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
NOZZLE EFFICIENCY
ROCKET BOOSTER
SOLID PROPELLANT ROCKET ENGINE
PHENOL
ABLATING MATERIAL

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