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Dielectric Resonator Antenna
Navy SBIR 2009.3 - Topic N093-173 NAVAIR - Mrs. Janet McGovern - [email protected] Opens: August 24, 2009 - Closes: September 23, 2009 N093-173 TITLE: Dielectric Resonator Antenna TECHNOLOGY AREAS: Air Platform, Sensors ACQUISITION PROGRAM: PMA290, Maritime Patrol and Reconnaissance Aircraft Program OBJECTIVE: Design and develop a multimode dielectric resonator antenna (DRA) or antennas capable of operating in the frequency band of 30 MHz to 2 GHz that can cover some or all of the current VHF/UHF line-of-sight (LOS) communications, UHF satellite communications, L-band and GPS functions requirements that can be used on a Navy aircraft. Proposed concepts should demonstrate improvement in either size or RF performance over the current antennas. DESCRIPTION: Currently, naval aircraft are covered with many antennas for VHF/UHF LOS communications, UHF satellite communications, L-band and GPS functions. Some of these antennas are of the blade type whose bandwidths are difficult to extend and whose form can impact the flight characteristics of the aircraft and create an ice accumulation hazard. Other, low profile, designs are usually cavity-backed requiring significant protrusion into the slipstream outside the aircraft or significant hull penetration inside the aircraft to accommodate the cavity whose bandwidths are also difficult to extend. There is a need to investigate alternate antenna technologies to ultimately condense some of these functions into a single structure to free up space for future additions, alleviate some of the interference between the antennas as well as reduce the size of existing antennas. Innovative concepts are sought that will demonstrate gain, pattern shape, polarization, power handling capabilities and VSWR potentially achievable by DRAs. Demonstration of all of these characteristics is not required although a successful proposal will incorporate as many as possible. As a guide, the antenna requirements of the current antenna technology is given below: VHF/UHF LOS communications: UHF satellite communications: L-Band: GPS: The design can be above the mold line or below. Primary constraints are weight and surface area consumed as weight allowance and surface area are always at a premium on any aircraft. It can be assumed that isolation will be handled by separate circuitry but each function should have a separate RF connector. PHASE I: Demonstrate feasibility of proposed DRA concept using either computer modeling and/or laboratory test with limited measured data. PHASE II: Develop, fabricate and demonstrate prototype (lab model) DRA to design goals. PHASE III: Transition developed antenna technology to fleet via airborne integration, operation, evaluation and production assuming sponsorship is secured from NAVAIR aircraft program. PRIVATE SECTOR COMMERCIAL POTENTIAL/DUAL-USE APPLICATIONS: Technology developed under this effort will have potential applications to unmanned air/surface/sea vehicles, multi-mission aircraft or any military aircraft or commercial aircraft where multiple antennas are used and space is limited. REFERENCES: 2. Y. Kobayashi and T. Tanaka, IEEE Trans Microwave Theory Tech., vol. MTT-28 (1980): 1077. 3. Y. Kobayashi and M. Miura, IEEE MTT-S Int. Microwave Symp. Dig. (1984): 184 4. K. M. Luk and K. W. Leung, Dielectric Resonator Antennas, J. R. James (ed.), (Baldock, Hertfordshire, UK: Research Studies Press Ltd., 2003). 5. A. Petosa, Dielectric Resonator Antenna Handbook, (Artech House, 2007). KEYWORDS: Antenna; Wide-band antenna; Dielectric resonator; Communications; Navigation; Satellite
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