Abstract
A microwave refractometer has been developed for use in a Type L-20 ``Beaver'' single-engine light aircraft. A two-channel recording system is used providing simultaneous profile and turbulence records with rms noise levels of approximately 0.05 and 0.01 N unit, respectively. Power requirement is 25 amperes at 28 volts dc, and installation requires one-half hour for two men. No structural modification of the aircraft is required. The results of flight tests are presented.
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