NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Creep behavior of tungsten/niobium and tungsten/niobium-1 percent zirconium compositesThe creep behavior and microstructural stability of tungsten fiber reinforced niobium and niobium 1 percent zirconium was determined at 1400 and 1500 K in order to assess the potential of this material for use in advanced space power systems. The creep behavior of the composite materials could be described by a power law creep equation. A linear relationship was found to exist between the minimum creep rate of the composite and the inverse of the composite creep rupture life. The composite materials had an order of magnitude increase in stress to achieve 1 percent creep strain and in rupture strength at test temperatures of 1400 and 1500 K compared to unreinforced material. The composite materials were also stronger than the unreinforced materials by an order of magnitude when density was taken into consideration. Results obtained on the creep behavior and microstructural stability of the composites show significant potential improvement in high temperature properties and mass reduction for space power system components.
Document ID
19880009323
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Petrasek, Donald W.
(NASA Lewis Research Center Cleveland, OH, United States)
Titran, Robert H.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1988
Subject Category
Metallic Materials
Report/Patent Number
NAS 1.15:100804
DOE/NASA/16310-5
E-3984
NASA-TM-100804
Report Number: NAS 1.15:100804
Report Number: DOE/NASA/16310-5
Report Number: E-3984
Report Number: NASA-TM-100804
Accession Number
88N18707
Funding Number(s)
PROJECT: RTOP 586-01-11
CONTRACT_GRANT: DE-AI03-86SF-16310
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available