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Low-Loss Ferrite Components for NASA Missions
Title: Principal Investigator
Phone: (434) 409-4044
Title: Business Official
Phone: (434) 409-4044
Ferrite based isolators and circulators have been successfully demonstrated at microwave, millimeter-wave and submillimeter-wave frequencies. These components are nonreciprocal and thus highly useful for controlling standing waves and directing signal flow in frequency multiplier cascades, heterodyne, radar, radiometer, and other systems commonly deployed by NASA. However, at the higher frequencies the performance is degraded in terms of bandwidth and loss which severely limits their usefulness.
Although there is a demonstrable need for these components, there are relatively few vendors. Most of the commercially available components were developed more than forty years ago and there has been little effort at modernization. Recent advances reported in the literature suggest that the loss in Faraday rotation isolators can be significantly reduced. Using modern electromagnetic simulation tools, we propose to design millimeter-wave and sub-millimeter-wave ferrite components that exhibit significantly reduced loss, and improved power handling and bandwidth.
Initial work on the development of a W-band isolator is underway. Ferrite cores have been manufactured and the impedance matching structures have been designed. We plan to demonstrate the effectiveness of our approach within the six month timeframe of the SBIR Phase I program. We have also successfully modeled Y-junction circulators that accurately predict performance similar to those available in the commercial market and are now working on several approaches to increase the bandwidth of these devices. A preliminary design operating at 160 GHz has been completed. In the Phase I program, the design will be refined, built and tested. Beyond Phase I, our goal is to develop a full line of ferrite components operating from 75 GHz to over 320 GHz with significantly improved performance over the current state-of-the-art.
* Information listed above is at the time of submission. *