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Materials for Aerospace Antennas and Radomes
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English
Abstract
This paper presents information compiled on the temperatures encountered by reentry and high performance aircraft, the metals and dielectrics useful for antennas and radome applications, and the effects of high temperature on the performance of these assemblies.
Authors
Citation
Buranich, G., "Materials for Aerospace Antennas and Radomes," SAE Technical Paper 660663, 1966, https://doi.org/10.4271/660663.Also In
References
- Buranich, Godfrey F. “Design Handbook for High Temperature Aerospace Antennas,” October 1965
- Marks, C. D. “Heat Protection by Radiative Heat Rejection,” Ninth Symposium on Ballistic Missile and Space Technology II Aerospace Corp. August 1964
- Johnston, E. W. “Advanced X-15 Research Airplane” Composite Research Panel, Minutes of Meeting November 1963 Johns Hopkins University
- Minges, M. L. “Thermal Transport Properties of Materials,” Air Force Materials Symposium 1965
- Walton J. D. Poulos, N. E. “Slip Cast Fused Slicia,” Air Force Materials Laboratory October 1964
- Krah, J. W. “High Temperature Telemetry Antennas for ASSET,” Proc. OSU-RTD Symposium on Electormagnetic Windows IV Ohio State University June 1964