NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Application of Ablation to a High Chamber Pressure Rocket EngineAblation cooling in rocket engine with combustion chamber liner and nozzle constructed of silica phenolic ablative material
Document ID
19710029273
Acquisition Source
Headquarters
Document Type
Contractor Report (CR)
Authors
Brecheisen, A. W. (Purdue Univ. West Lafayette, IN, United States)
Ehresman, C. M. (Purdue Univ. West Lafayette, IN, United States)
Date Acquired
August 6, 2013
Publication Date
August 1, 1971
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-CR-120798
Accession Number
71N38749
Funding Number(s)
CONTRACT_GRANT: NGR-15-005-058
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available