NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Experimental evaluation of six ablative-material thrust chambers as components of storable-propellant rocket enginesTest firing evaluation of six ablative-material thrust chambers as components of storable propellant rocket engines
Document ID
19670026445
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Shinn, A. M., Jr. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1967
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TN-D-3945
Report Number: NASA-TN-D-3945
Accession Number
67N35774
Funding Number(s)
CONTRACT_GRANT: 128-31-03-01-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
COMBUSTION CHAMBER
LIQUID PROPELLANT ROCKET ENGINE
STORABLE PROPELLANT
ABLATING MATERIAL

Related Records

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