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THE RADIATION EFFECTS TESTING OF AIRCRAFT SYSTEMS
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English
Abstract
The evaluation of aircraft systems’ performance characteristics in a radiation environment are discussed. Environmental factors and requirements for conducting irradiations on dynamic systems are emphasized. Some major requirements for test facility capabilities are presented and a facility meeting these requirements is described. The facility functions are detailed by following a test item through the sequence of operations for a typical test program.
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Citation
MILLER, M. and LIEBSCHUTZ, A., "THE RADIATION EFFECTS TESTING OF AIRCRAFT SYSTEMS," SAE Technical Paper 580075, 1958, https://doi.org/10.4271/580075.Also In
References
- Krasnow “Determination of Testing Schemes for ANP Weapons System Materiel,” WADC TN 57-185, May 1957
- Segrest, R. H. “Strain Gage Transducer Irradiation Test Program” NR-35
- Andrews, R. D. Tobolsky, A. V. Hanson, E. E. “The Theory of Permanent Set at Elevated Temperatures in Natural and Synthetic Rubber Vulcanizates,” High Polymer Physics, Ramsen Press, page 215 1948 American Institute of Physics
- Martens, J. H. Minuth, F. G. “Neutron and Gamma Irradiation Facilities,” Technical Information Service U.S. AEC April 1957