1998 IEEE.
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IEEE Transactions on Antennas and Propagation
Volume 46 Number 10, October 1998
Table of Contents for this issue
Complete paper in PDF format
RF Characterization of an Inflatable Parabolic Torus Reflector Antenna for Space-Borne Applications
Robert A. Hoferer, Student Member, IEEE, and Yahya Rahmat-Samii, Fellow, IEEE
Page 1449.
Abstract:
Space-borne satellite applications provide a vast array of
services extending from global connectivity to earth observation
systems. The soil moisture radiation mission is a proposed space-borne
passive microwave system complementary to the existing earth observing
system operating at low microwave frequencies and requiring an antenna
with multibeam, high-beam efficiency, and dual polarization
capabilities. To achieve both the large reflector size and the multibeam
pattern at the operational frequencies an innovative multibeam reflector
antenna design was needed. Recent advances in inflatable antenna
technology has been proposed to overcome the launch vehicle size and
weight restrictions. This paper describes a novel offset parabolic torus
reflector antenna design that produces the desired multibeam pattern and
is compatible with the inflatable antenna technology. Using the system
requirements of this mission as an example, the design process for an
inflatable parabolic torus reflector antenna is outlined, the
development of suitable distortion models is given, and representative
RF characteristics are presented. These RF characteristics
include far-field patterns, beam contour patterns, beam efficiency, and
other key performance parameters. The development of an advanced
analytical modeling/numerical tool in support of the design effort is
also detailed.
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