NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Rocket Combustion Chambers Resist Thermal FatigueImproved design concept developed for combustion chambers for rocket engines, described in three reports. Provides compliance allowing unrestrained thermal expansion in circumferential direction. Compliance lengthens life of rocket engine by reducing amount of thermal deformation caused by repeated firings.
Document ID
19950065354
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Kazaroff, John M. (NASA Lewis Research Center, Cleveland, OH.)
Jankovsky, Robert S. (NASA Lewis Research Center, Cleveland, OH.)
Pavli, Albert J. (Sverdrup Technology, Inc.)
Date Acquired
August 17, 2013
Publication Date
April 1, 1995
Publication Information
Publication: NASA Tech Briefs
Volume: 19
Issue: 4
ISSN: 0145-319X
Subject Category
Fabrication Technology
Report/Patent Number
LEW-15766
Accession Number
95B10195
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Available Downloads

There are no available downloads for this record.

Related Records

IDRelationTitleA92-44509/TBSee AlsoAdvanced Tube-Bundle Rocket Thrust Chambers.
No Preview Available