Abstract
The ratio of specularly reflected to scattered power received by a radar altimeter is shown to be related to a parameter q = (4K2/σ0 ß2), where K is the Fresnel reflection coefficient, σ0 is the differential scattering coefficient, and ß is the effective beamwidth. The critical range of rms surface roughness is shown to be from 0.1 to 0.335 λ for examples from 100-ns-pulse aircraft radar to 10-ns-pulse spacecraft radar over water.

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