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Advancements in Structural Beryllium Technology
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English
Abstract
Development of structural beryllium technology at McDonnell comprising both hardware and study programs is discussed, including wing-box structures, F-4 and SST rudders, F-4 brakes, and crack propagation and damage tolerant design evaluations. Impediments to a more extensive use of beryllium are discussed and areas requiring further study and development defined.
Authors
Citation
Muehlberger, D., "Advancements in Structural Beryllium Technology," SAE Technical Paper 680330, 1968, https://doi.org/10.4271/680330.Also In
References
- Finn J. M. Koch L. C. Muehlberger D. E. “Design, Fabrication, and Testing of an Aerospace Plane Beryllium Wing-Box.” Final Report to Air Force Flight Dynamics Laboratory, AFFDL-TR-67-38 March 1967
- Finn J. M. Koch L. C. Muehlberger D. E. “Design, Fabrication, and Ground Testing of the F-4 Beryllium Rudder.” Final Report to Air Force Flight Dynamics Laboratory, AFFDL-TR-67-68 April 1967
- “Fabrication, Instrumentation, Flight Test, and Evaluation of an F-4 Beryllium Rudder.” Air Force Flight Dynamics Laboratory Contract No. F33615-67-C-1618 April 17 1967
- “Beryllium Structural Panels.” Air Force Flight Dynamics Laboratory Contract No. F33615-67-C-1266 Jan. 3 1967