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Rhenium Mechanical Properties and Joining TechnologyIridium-coated rhenium (Ir/Re) provides thermal margin for high performance and long life radiation cooled rockets. Two issues that have arisen in the development of flight Ir/Re engines are the sparsity of rhenium (Re) mechanical property data (particularly at high temperatures) required for engineering design, and the inability to directly electron beam weld Re chambers to C103 nozzle skirts. To address these issues, a Re mechanical property database is being established and techniques for creating Re/C103 transition joints are being investigated. This paper discusses the tensile testing results of powder metallurgy Re samples at temperatures from 1370 to 2090 C. Also discussed is the evaluation of Re/C103 transition pieces joined by both, explosive and diffusion bonding. Finally, the evaluation of full size Re transition pieces, joined by inertia welding, as well as explosive and diffusion bonding, is detailed.
Document ID
19970009605
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Reed, Brian D.
(NASA Lewis Research Center Cleveland, OH United States)
Biaglow, James A.
(NASA Lewis Research Center Cleveland, OH United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1996
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-TM-107317
AIAA Paper 96-2598
NAS 1.15:107317
E-10413
Meeting Information
Meeting: Joint Propulsion Conference
Location: Lake Buena Vista, FL
Country: United States
Start Date: July 1, 1996
End Date: July 3, 1996
Sponsors: American Society for Electrical Engineers, Society of Automotive Engineers, Inc., American Inst. of Aeronautics and Astronautics, American Society of Mechanical Engineers
Accession Number
97N15007
Funding Number(s)
PROJECT: RTOP 242-70-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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