Handout (296.7 kB)
A prototype lens was constructed and tested with the WCR in Laramie using a pole mounted trihedral corner reflector. The thickness of the 12" diameter lens turned out to be 4'' - much thinner than the height of 36" of a conventional grid reflector for the same application. This reduction in size, however, was achieved at the expense of performance. The lens reduced the sensitivity of the radar by about 5 dB and the isolation between the deflected and the direct beams was only 3 dB when the deflected beam was transmitted, making the lens a beam splitter rather than a beam switch. During airborne measurements, however, the difference in Doppler shift increases the isolation between the two beams to above 20 dB, making dual beam Doppler and reflectivity measurements still possible from an aircraft.
In November 2000 the lens was mounted in the KingAir and during two flights dual beam radar data were collected from ice clouds. The lens split the radar beam into the "side" and " side-aft" (beam pointed 45 deg aft in the horizontal plane) beams. The Doppler shifted returns from the two beams were distinct and clearly identifiable as the three times folded side-aft beam peak appeared near -13 m/s (indicating a radial Doppler velocity of -65.7 m/s), while the side beam peak was around -4 m/s. For 2-D Doppler velocity field analysis the centroid of each peak was tracked and for the estimation of the attenuation field using Stereorad processing, the power of the peaks was calculated.
This paper will describe the design and performance of the lens and present airborne dual Doppler and 95 GHz radar reflectivity measurements from ice clouds.