NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
An analytical method for determining the melt- layer thickness and regression rates for a hybrid or tribrid rocket motorAnalysis of fuel thermal conductivity effects on melt layer buildup and regression rates in hybrid and tribrid propellant rocket engines
Document ID
19700018038
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Drew, W. B. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1970
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TN-D-5699
Accession Number
70N27348
Funding Number(s)
CONTRACT_GRANT: 128-32-60-01-23
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