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Evaluation of Rhenium Joining MethodsCoupons of rhenium-to-Cl03 flat plate joints, formed by explosive and diffusion bonding, were evaluated in a series of shear tests. Shear testing was conducted on as-received, thermally-cycled (100 cycles, from 21 to 1100 C), and thermally-aged (3 and 6 hrs at 1100 C) joint coupons. Shear tests were also conducted on joint coupons with rhenium and/or Cl03 electron beam welded tabs to simulate the joint's incorporation into a structure. Ultimate shear strength was used as a figure of merit to assess the effects of the thermal treatment and the electron beam welding of tabs on the joint coupons. All of the coupons survived thermal testing intact and without any visible degradation. Two different lots of as-received, explosively-bonded joint coupons had ultimate shear strengths of 281 and 310 MPa and 162 and 223 MPa, respectively. As-received, diffusion-bonded coupons had ultimate shear strengths of 199 and 348 MPa. For the most part, the thermally-treated and rhenium weld tab coupons had shear strengths slightly reduced or within the range of the as-received values. Coupons with Cl03 weld tabs experienced a significant reduction in shear strength. The degradation of strength appeared to be the result of a poor heat sink provided during the electron beam welding. The Cl03 base material could not dissipate heat as effectively as rhenium, leading to the formation of a brittle rhenium-niobium intermetallic.
Document ID
19960002343
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Reed, Brian D.
(NASA Lewis Research Center Cleveland, OH, United States)
Morren, Sybil H.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1995
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 95-2397
NASA-TM-107055
NAS 1.15:107055
E-9903
Report Number: AIAA PAPER 95-2397
Report Number: NASA-TM-107055
Report Number: NAS 1.15:107055
Report Number: E-9903
Meeting Information
Meeting: Joint Propulsion Conference and Exhibit
Location: San Diego, CA
Country: United States
Start Date: July 10, 1995
End Date: July 12, 1995
Sponsors: AIAA, ASME, SAE, and ASEE
Accession Number
96N12351
Funding Number(s)
PROJECT: RTOP 232-02-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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