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Analytical and experimental study of ablation material for rocket engine application Final reportTechniques for rating performance of ablative materials in liquid-propellant rocket engines
Document ID
19660019255
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Flood, D. T. (Itek Corp. Palo Alto, CA, United States)
Kendall, R. M. (Itek Corp. Palo Alto, CA, United States)
Rindal, R. A. (Itek Corp. Palo Alto, CA, United States)
Date Acquired
August 3, 2013
Publication Date
May 15, 1966
Subject Category
Propulsion Systems
Report/Patent Number
VIDYA-201
NASA-CR-54757
Report Number: VIDYA-201
Report Number: NASA-CR-54757
Accession Number
66N28545
Funding Number(s)
CONTRACT_GRANT: NAS7-218
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ABLATING MATERIAL
LIQUID PROPELLANT ROCKET ENGINE
THERMAL INSULATION

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