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Conformal Omni-Directional Antenna Design for Unmanned Aerial Vehicle (UAV)

Award Information
Agency: Department of Defense
Branch: Army
Contract: W15P7T-09-C-S454
Agency Tracking Number: A082-112-1384
Amount: $119,455.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: A08-112
Solicitation Number: 2008.2
Timeline
Solicitation Year: 2008
Award Year: 2009
Award Start Date (Proposal Award Date): 2008-12-09
Award End Date (Contract End Date): 2009-06-09
Small Business Information
4865 Sterling Drive
Boulder, CO 80301
United States
DUNS: 125961123
HUBZone Owned: No
Woman Owned: Yes
Socially and Economically Disadvantaged: No
Principal Investigator
 Farzin Lalezari
 Principal Investigator
 (303) 449-5211
 flalezari@firstrf.com
Business Contact
 Theresa Boone
Title: Chief Operating Officer
Phone: (303) 449-5211
Email: tboone@firstrf.com
Research Institution
N/A
Abstract

The proliferation of Unmanned Aerial Vehicles (UAVs) in DoD’s fleet has created a serious need for lightweight, airborne conformal antennas that cover numerous frequency bands. Shadow 200 is a great example of a high performance, exceptionally versatile UAV system which is finding use among nearly all DoD services. This airframe’s ever-expanding set of functions requires a fresh approach to antenna design that is a departure from the traditional function-specific bolt-on antenna. There is an urgent demand for low-frequency vertically polarized antennas for the Shadow UAV and similarly sized vehicles. Commercially available aviation antenna products are too heavy with an unacceptably large aerodynamic cross section for use aboard Shadow. FIRST RF’s proposed antenna technology uses planar wideband antenna apertures to provide a vertically polarized omni-directional beam. The proposed concept combines the practicality of existing antenna designs with a novel application approach to provide airborne SINCGARS and EPLRS coverage from a conformal antenna. FIRST RF’s proposed antenna design exceeds the gain specification of -15 dBi by a wide margin, and yet produces no drag to the vehicle and requires no protrusion into the existing airframe. This technology holds tremendous commercialization potential due to its practicality, conformality, high gain and wide bandwidth.

* Information listed above is at the time of submission. *

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