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Ka-band Doppler Scatterometer for Measurements of Ocean Vector Winds and Surface Currents (DopplerScatt)
Completed
TRL 6 (started at 3, targeting 6)
Description
Ocean surface currents impact heat transport, surface momentum and gas fluxes, ocean productivity and marine biological communities. Ocean currents also have social impacts on shipping and disaster management (e.g., oil spills). There is an intrinsic two-way coupling between ocean currents and surface winds and concurrent measurements of the two enable the understanding of the relevant air-sea interaction. The ability to simultaneously measure winds and currents improves the accuracy of both individual measurements. To date, measurements of ocean surface currents and winds have not been made simultaneously. Currently there are no planned global direct measurements of ocean surface currents and winds (SWOT and altimeters measure geostrophic components of ocean currents). We propose to build the first demonstrator instrument of the new measurement technique capable of measuring both currents and winds using a compact radar instrument that will be developed in this project. The instrument is a spinning Ka-band pencil-beam Doppler scatterometer system (DopplerScatt). The proposed development will demonstrate measurements that can be scaled to wide swath spaceborne observations using a single cost-effective instrument. The proposed work will be divided into three major tasks: 1) design and build of the radar for a spinning antenna configuration, closed-loop calibration and a digital back-end system for on-board processing, 2) end-to-end system test and integration on the airborne platform and 3) demonstration of achievable accuracy for joint vector wind and current retrieval through a designed airborne experiment. The last year of the proposed 3-year duration will be used for instrument integration and testing, aircraft installation and engineering flights. The details of the work plan and cost assumptions are provided in Section 6. The entry TRL for DopplerScatt will be 3 while the exit TRL will be 6 upon completion of the engineering checkout and validation flights.
Benefits
Enabling lower cost innovative remote sensing instrument development from concept through breadboard and demonstration
Details
| Technology area | Sensors and Instruments > Remote Sensing Instruments and Sensors > Microwave, Millimeter Waves, and Submillimeter Waves |
| Program | Instrument Incubator (IIP) |
| Lead organization | NASA Headquarters, Washington, DC |
| Start date | 2014-05-01 |
| End date | 2017-07-31 |
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