ADAPTIVE ELECTRONICALLY STEERABLE ARRAY (AESA) SYSTEM FOR INTERCEPTOR RF TARGET ENGAGEMENT AND COMMUNICATIONS
First Claim
1. An adaptive electronically steerable array (AESA) system suitable for use on an interceptor, said interceptor comprising a plurality of aerodynamic control surfaces position about an airframe, each control surface having a forward-facing surface, said AESA system comprising:
- a plurality of arrays, each comprising a plurality of radiating elements, each said array configured for placement on the forward-facing surface of a different one of said plurality of aerodynamic control surfaces;
a plurality of RF transmissive radome elements, each radome element configured for placement over one of said arrays, each said radome element having an aerodynamic shape complementary to said aerodynamic control surface; and
control circuitry to configure the arrays for RF target engagement.
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Accused Products
Abstract
An AESA system comprises a plurality of arrays, each comprising a plurality of radiating elements, each array configured for placement on a forward-facing surface of a different one of a plurality of aerodynamic control surfaces on an interceptor. A plurality of RF transmissive radome elements, each having an aerodynamic shape complementary to the aerodynamic control surface, are placed over one of the arrays. Control circuitry configures the arrays, independently or in concert, for RF target engagement and communication. Additional arrays may be positioned on side or aft-facing surfaces of the aerodynamic control surfaces for RF communication. The AESA system may be paired with an ER system for dual-mode operation.
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Citations
20 Claims
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1. An adaptive electronically steerable array (AESA) system suitable for use on an interceptor, said interceptor comprising a plurality of aerodynamic control surfaces position about an airframe, each control surface having a forward-facing surface, said AESA system comprising:
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a plurality of arrays, each comprising a plurality of radiating elements, each said array configured for placement on the forward-facing surface of a different one of said plurality of aerodynamic control surfaces; a plurality of RF transmissive radome elements, each radome element configured for placement over one of said arrays, each said radome element having an aerodynamic shape complementary to said aerodynamic control surface; and control circuitry to configure the arrays for RF target engagement. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13)
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14. An interceptor comprising:
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an airframe; a plurality of aerodynamic control surfaces position about the airframe, each control surface having a forward-facing surface, an adaptive electronically steerable array (AESA) system comprising a plurality of arrays, each comprising a plurality of radiating elements, each said array positioned on the forward-facing surface of a different one of said plurality of aerodynamic control surfaces; a plurality of RF transmissive radome elements placed over different ones of said arrays, each said radome element having an aerodynamic shape complementary to said aerodynamic control surface; and control circuitry to configure the arrays for RF target engagement. - View Dependent Claims (15, 16)
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17. A method of RF target engagement comprising:
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positioning arrays on the forward-facing surfaces of a plurality of aerodynamic control surfaces positioned about an interceptor, each array comprising a plurality of radiating elements that together define an adaptive electronically steerable array (AESA) system; placing a plurality of RF transmissive radome elements over different ones of said arrays, each said radome element having an aerodynamic shape complementary to said aerodynamic control surface; and configuring the arrays for RF target engagement. - View Dependent Claims (18, 19, 20)
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Specification