NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Liquid rocket engine fluid-cooled combustion chambersA monograph on the design and development of fluid cooled combustion chambers for liquid propellant rocket engines is presented. The subjects discussed are (1) regenerative cooling, (2) transpiration cooling, (3) film cooling, (4) structural analysis, (5) chamber reinforcement, and (6) operational problems.
Document ID
19730022965
Acquisition Source
Legacy CDMS
Document Type
Special Publication (SP)
Date Acquired
September 2, 2013
Publication Date
April 1, 1972
Subject Category
Propulsion Systems
Report/Patent Number
NASA-SP-8087
Report Number: NASA-SP-8087
Accession Number
73N31697
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