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Titanium Fabrication Techniques for the XB-70 and Beyond
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English
Abstract
The following discussion outlines the applications of titanium technology to the XB-70 program, touching on alloy applications to solve specific design problems, and describing fabrication processes and sequences. A brief discussion of a space booster application, a sine wave welded crossbeam, is included. The discussion is concluded by the description of new titanium applications as diffusion bonded structure and as composite materials.
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Citation
Reinsch, W., "Titanium Fabrication Techniques for the XB-70 and Beyond," SAE Technical Paper 660650, 1966, https://doi.org/10.4271/660650.Also In
References
- Jackson, J. D. Boyd, W. K. “The Stress-corrosion and Accelerated Crack Propagation Behavior of Titanium and Titanium Alloys.” DMIC Technical Note Battelle Memorial Institute February 1 1966
- Lewis, G. B. et al “Final Report - Experimental Titanium Crossbeam Manufacturing Technology.” North American Aviation, Inc November 12 1965
- Wood, R. A. “The Ti-8Al-1Mo-1V Alloy.” Battelle Memorial Institute April 1 1965
- Manzone, M. G. “Titanium Alloys with Molybdenum.” Climax Molybdenum Co 1966
- Vagi, J J. et al “Welding Procedures for Titanium and Titanium Alloys.” NASA Octob0er 1965
- Klimmek, N. Robelotto, R. Sidbeck, P. “Residual Weld Stress in Titanium Fusion Weldments.” North American Aviation, Inc 29 September 1965
- Wagner, H. J. “Fiber-Reinforced Metals,” DMIC Review, Battelle Memorial Institute June 24 1966
- Sinizer, D. I. Toy, A. Atteridge, D. G. “Development of the Diffusion Bonding Process as a Method to Produce Fibrous Reinforced Metal Matrix Composite Materials.” North American Aviation, Inc February 15 – May 15 1966