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New main reflector, subreflector and dual chamber concepts for compact range applicationsA compact range is a facility used for the measurement of antenna radiation and target scattering problems. Most presently available parabolic reflectors do not produce ideal uniform plane waves in the target zone. Design improvements are suggested to reduce the amplitude taper, ripple and cross polarization errors. The ripple caused by diffractions from the reflector edges can be reduced by adding blended rolled edges and shaping the edge contour. Since the reflected edge continues smoothly from the parabola onto the rolled surface, rather than being abruptly terminated, the discontinuity in the reflected field is reduced which results in weaker diffracted fields. This is done by blending the rolled edges from the parabola into an ellipse. An algorithm which enables one to design optimum blended rolled edges was developed that is based on an analysis of the continuity of the surface radius of curvature and its derivatives across the junction. Futhermore, a concave edge contour results in a divergent diffracted ray pattern and hence less stray energy in the target zone. Design equations for three-dimensional reflectors are given. Various examples were analyzed using a new physical optics method which eliminates the effects of the false scattering centers on the incident shadow boundaries. A Gregorian subreflector system, in which both the subreflector and feed axes are tilted, results in a substantial reduction in the amplitude taper and cross polarization errors. A dual chamber configuration is proposed to eliminate the effects of diffraction from the subreflector and spillover from the feed. A computationally efficient technique, based on ray tracing and aperture integration, was developed to analyze the scattering from a lossy dielectric slab with a wedge termination.
Document ID
19880003116
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Pistorius, C. W. I.
(Ohio State Univ. Columbus, OH, United States)
Burnside, W. D.
(Ohio State Univ. Columbus, OH, United States)
Date Acquired
September 5, 2013
Publication Date
August 1, 1987
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NASA-CR-181506
OSU-716148-22
NAS 1.26:181506
Accession Number
88N12498
Funding Number(s)
CONTRACT_GRANT: NSG-1613
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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