A proposed microstrip Yagi antenna would operate at a frequency of 8.4 GHz (which is in the X band) and would feature a mechanically simpler, more elegant design, relative to a prior L-band microstrip Yagi antenna. In general, the purpose of designing a microstrip Yagi antenna is to combine features of a Yagi antenna with those of a microstrip patch to obtain an antenna that can be manufactured at low cost, has a low profile, and radiates a directive beam that, as plotted on an elevation plane perpendicular to the antenna plane, appears tilted away from the broadside. Such antennas are suitable for flush mounting on surfaces of diverse objects, including spacecraft, aircraft, land vehicles, and computers.

Stated somewhat more precisely, what has been proposed is a microstrip antenna comprising an array of three Yagi elements. Each element would include four microstrip-patch Yagi subelements: one reflector patch, one driven patch, and two director patches. To obtain circular polarization, each driven patch would be fed by use of a dual offset aperture-coupled feed featuring bow-tie-shaped apertures (see figure). The selection of the dual offset bow-tie aperture geometry is supported by results found in published literature that show that this geometry would enable matching of the impedances of the driven patches to the 50-Ω impedance of the microstrip feedline while maintaining a desirably large front-to-back lobe ratio.
This work was done by Ronald Pogorzelski and Jaikrishna Venkatesan of Caltech for NASA's Jet Propulsion Laboratory.
In accordance with Public Law 96-517, the contractor has elected to retain title to this invention. Inquiries concerning rights for its commercial use should be addressed to:
Innovative Technology Assets Management
JPL
Mail Stop 202-233
4800 Oak Grove Drive
Pasadena, CA 91109-8099
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Refer to NPO-41791, volume and number of this NASA Tech Briefs issue, and the page number.
This Brief includes a Technical Support Package (TSP).

Microstrip Yagi Antenna With Dual Aperture-Coupled Feed
(reference NPO-41791) is currently available for download from the TSP library.
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Overview
The document discusses the development of a Microstrip Yagi Antenna with a Dual Aperture-Coupled Feed, originally designed at NASA's Jet Propulsion Laboratory (JPL) by Dr. John Huang. This innovative antenna is specifically tailored for X-band operation at 8.4 GHz and aims to achieve circular polarization, which is essential for various aerospace applications.
The original design utilized a coaxial probe feed, which posed significant electrical and mechanical challenges, particularly in matching the coaxial line to the antenna due to parasitic effects. Additionally, the coaxial feed required complex integration through multiple substrates, complicating the overall design. To address these issues, the new design employs a dual offset aperture-coupled feed, which allows for a more elegant and planar implementation of the antenna and its associated feed electronics.
The microstrip Yagi array consists of three elements, each featuring one reflector patch, one driven patch, and two director patches. The dual bow-tie shaped aperture-coupled feed enhances coupling between the microstrip feedline and the driven patch element, facilitating a better match to a 50-Ohm microstrip feedline while maintaining a low front-to-back lobe ratio. This design choice is crucial for optimizing antenna performance and reducing cross-polarized radiation, which can be problematic in other feeding techniques.
The document highlights the novelty of this design, emphasizing its potential for integration into landed assets' panels, making it suitable for various applications in aerospace technology. The use of a bow-tie shaped aperture is particularly noted for its ability to balance coupling efficiency and radiation pattern quality.
Overall, the Microstrip Yagi Antenna with Dual Aperture-Coupled Feed represents a significant advancement in antenna technology, addressing the limitations of previous designs while providing a solution that is both efficient and practical for modern aerospace applications. The document serves as a technical support package under NASA's Commercial Technology Program, aiming to disseminate aerospace-related developments with broader technological, scientific, and commercial implications.

