Journal
COMPOSITES SCIENCE AND TECHNOLOGY
Volume 105, Issue -, Pages 96-101Publisher
ELSEVIER SCI LTD
DOI: 10.1016/j.compscitech.2014.10.004
Keywords
Functional composites; Glass fibers; Smart materials; Electrical properties; Modelling
Categories
Funding
- Low Observable Technology Research Center program of the Defense Acquisition Program Administration and Agency for Defense Development
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In this paper, a circuit analog (CA) absorber consisting of a periodic, resistive-pattern sheet and glass-fiber/epoxy composite spacer; for integration into the leading edge of a wing-shaped structure, was introduced along with practical steps to take from design to fabrication. The CA absorber was designed in a flat-plate shape for the X-band (8.2-12.4 GHz). To fabricate a periodic-resistive-pattern surface compatible with a 180 degrees C autoclave process, a carbon-based conducting material was used. The reflection loss of this flat-plate CA absorber was measured with an X-band, free-space measurement system. A leading edge for a wing-shaped structure incorporating the new CA absorber was designed and fabricated based on data from a flat-plate-design CA absorber. The integrated leading edge was mounted on a wing-box, and its echo-RCS was measured in an anechoic chamber. When the CA absorber was applied to the leading edge of the wing-shaped structure, the echo-RCS level measured by compact range showed a reduction of about 10 dB in most of the X-band, in both polarizations. From a practical point of view, these results confirmed that CA absorbent materials have great potential in radar absorbing structures for stealth aircraft. (C) 2014 Elsevier Ltd. All rights reserved.
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