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Multibeam communications satellite

Assignee: International Telecommunications Satellite Organization
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Filing: 1978-04-20
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Granted: 1980-05-06
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Expires: 1998-04-20
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Abstract

Abstract A multibeam communications satellite uses a dish-shaped reflector whose surface is a surface of revolution generated by rotating a plane parabola about an axis of revolution located in the plane of the parabola but angularly displaced from the axis of symmetry thereof. The line of revolution of the focal point of the parabola defines a focal circle, and a feed located on the focal circle will illuminate an area lying on a circle near the edge of the earth's apparent disc. Since every plane in which the axis of revolution lies is a plane of symmetry, the antenna exhibits good cross polarization cancellation, making the satellite particularly useful in frequency reuse communications systems.

Inventors

  • 👤 George R. Welti

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-28 15:20
CPC Classifications
H; H01; H01Q; H01Q19/00; H01Q19/10; H01Q19/12; H01Q19/17; H01Q25/00; H01Q25/007; Y; Y10; Y10S; Y10S343/00; Y10S343/02

Claims Analysis

Total Claims: 6
Claim 1
Independent Claim 82 words
In a multibeam communications satellite of the type having an antenna which comprises a reflector and a plurality of feeds for directing radiation at different areas of the surface of said reflector for redirection to various points on earth, the improvement comprising said reflector surface being described by a plane parabolic generating curve rotated about an axis of revolution which is coplanar with said generating curve but angularly displaced from the axis of symmetry thereof by an angle of less than 12°.
Claim 2
Dependent Claim 82 words
In a multibeam communications satellite of the type having an antenna which comprises a reflector and a plurality of feeds for directing radiation at different areas of the surface of said reflector for redirection to various points on earth, the improvement comprising said reflector surface being described by a plane parabolic generating curve rotated about an axis of revolution which is coplanar with said generating curve but angularly displaced from the axis of symmetry thereof by an angle of less than 12°.
Claim 3
Dependent Claim 69 words
The improvement in a multibeam communications satellite according to claim 1 wherein the size of the angle between said axis of revolution and said axis of said symmetry is chosen so that when said axis of revolution is aligned with the center of the earth's apparent disc, the axis of symmetry of said parabola defines a circle on said disc as it is rotated about said axis of revolution.
Claim 4
Dependent Claim 17 words
The improvement in a multibeam communications satellite according to claim 2 wherein said angle is approximately 8°.
Claim 5
Dependent Claim 37 words
The improvement in a multibeam communications satellite according to claim 2 wherein said plurality of feeds are positioned substantially within a region defined by said axis of symmetry as it is rotated about said axis of revolution.
Claim 6
Dependent Claim 39 words
The improvement in a multibeam communications satellite according to claim 1 wherein the plurality of feeds are positioned on a conical surface defined by the focal line of said parabola as it is rotated about said axis of revolution.

References Cited (Backward Citations)

US3922682A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1983-05-06 1983-11-05 1984-05-06 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1987-05-06 1987-11-05 1988-05-06 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1991-05-06 1991-11-05 1992-05-06 $7700.00 Window Closed / Lapsed

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