2007
DOI: 10.1109/tap.2007.905835
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Back-to-Back Reflector Antennas With Reduced Moment of Inertia for Spacecraft Spinning Platforms

Abstract: A back-to-back reflector antenna system with reduced moment of inertia is proposed in order to address the demanding problem of supporting large reflector antennas on spinning platforms. The configuration provides additional potential advantages, such as reducing the spinning speed by half for a given sampling rate when both back-to-back reflectors are utilized. Geometrical parameters of the reflector are determined such that the moment of inertia of the rotating system is reduced. It is shown that these back-… Show more

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Cited by 14 publications
(8 citation statements)
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“…With the primary feed model defined by (4) and linear phase errors given by (2), in (2) changes from 0 to 1 with a step of 0.25 to include the phase errors in both TE and TE modes. The secondary far-field crosspolar components are numerically calculated at both diagonal and asymmetry planes, i.e., and 90 .…”
Section: A Linear Phase Errormentioning
confidence: 99%
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“…With the primary feed model defined by (4) and linear phase errors given by (2), in (2) changes from 0 to 1 with a step of 0.25 to include the phase errors in both TE and TE modes. The secondary far-field crosspolar components are numerically calculated at both diagonal and asymmetry planes, i.e., and 90 .…”
Section: A Linear Phase Errormentioning
confidence: 99%
“…This case can be interpreted as a dual-mode feed having different phase center locations for each individual mode. With the linear phase errors described by (2), the secondary cross polarization levels are calculated at both and 90 planes as before. The results are depicted in Fig.…”
Section: B Quadratic Phase Errormentioning
confidence: 99%
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“…A novel approach to overcome the aforementioned drawbacks is to use the back-to-back reflector structure [7][8][9], as shown in Figure 1. This gravitationally balanced configuration utilizes two identical reflectors, mounted back-to-back on a spinning platform.…”
Section: Introductionmentioning
confidence: 99%
“…Later, Jacobson [6] presented two solutions: one a dual-mode rectangular horn and the other a linear array of small aperture round waveguide feeds, with their axes parallel to the optical axis of the offset reflector, to reduce cross polarization in the offset reflector antenna. The tri-mode feed design has been recently revisited by [7] for balanced back-to-back reflectors with a reduced moment of inertia.…”
mentioning
confidence: 99%