NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Due to the lapse in federal government funding, NASA is not updating this website. We sincerely regret this inconvenience.

Back to Results
Conventionally cast and forged copper alloy for high-heat-flux thrust chambersThe combustion chamber liner of the space shuttle main engine is made of NARloy-Z, a copper-silver-zirconium alloy. This alloy was produced by vacuum melting and vacuum centrifugal casting; a production method that is currently now available. Using conventional melting, casting, and forging methods, NASA has produced an alloy of the same composition called NASA-Z. This report compares the composition, microstructure, tensile properties, low-cycle fatigue life, and hot-firing life of these two materials. The results show that the materials have similar characteristics.
Document ID
19870007469
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Kazaroff, John M.
(NASA Lewis Research Center Cleveland, OH, United States)
Repas, George A.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
February 1, 1987
Subject Category
Metallic Materials
Report/Patent Number
NASA-TP-2694
NAS 1.60:2694
E-3304
Report Number: NASA-TP-2694
Report Number: NAS 1.60:2694
Report Number: E-3304
Accession Number
87N16902
Funding Number(s)
PROJECT: RTOP 506-42-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available