Small volume dual offset reflector antenna
First Claim
1. A dual offset dual reflector antenna for a satellite-to-satellite communication system, said antenna comprising:
- a main reflector having a paraboloidal shape, comprising a segment of a paraboloid and defining a paraboloid focal axis, a focal length and a focal point, comprising a terminus of said focal length, located on said paraboloid focal axis;
a subreflector having a hyperboloidal shape, comprising a segment of a hyperboloid and defining first and second foci to said hyperboloidal segment;
said sub-reflector being positioned with said first foci in coincident position with said focal point and said second foci being located at a predetermined position above said focal axis;
a microwave feed horn having an aperture and a feed axis;
said microwave feed horn aperture being positioned at said second foci and above said paraboloid focal axis with said feed horn axis being oriented parallel to said paraboloid focal axis and intersecting said subreflector; and
said focal length bearing a ratio relationship to said diameter of said main reflector that is less than one.
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Abstract
The problem of reducing the size of a dual offset Cassegrain reflector type microwave antenna without adversely affecting performance while retaining the simplicity of the main reflector'"'"'s (1) and subreflector'"'"'s (3) traditional simple surface curvatures is solved by having the paraboloidal shaped main reflector'"'"'s focal length, fm, and diameter, D, fulfil the criteria that the ratio of fm to D is less than 1.0; and in which the hyperboloidal shaped subreflector (3) is oriented so that its left foci, at which the microwave feed (5) aperture is placed, lies above the main reflector'"'"'s focal axis. It'"'"'s subreflector subtends an angular arc about the focal point that is slightly larger than the corresponding arc subtended by the main reflector. The elegance of the compact antenna is demonstrated by improved performance, attaining efficiencies in excess of seventy three percent.
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Citations
13 Claims
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1. A dual offset dual reflector antenna for a satellite-to-satellite communication system, said antenna comprising:
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a main reflector having a paraboloidal shape, comprising a segment of a paraboloid and defining a paraboloid focal axis, a focal length and a focal point, comprising a terminus of said focal length, located on said paraboloid focal axis; a subreflector having a hyperboloidal shape, comprising a segment of a hyperboloid and defining first and second foci to said hyperboloidal segment; said sub-reflector being positioned with said first foci in coincident position with said focal point and said second foci being located at a predetermined position above said focal axis; a microwave feed horn having an aperture and a feed axis; said microwave feed horn aperture being positioned at said second foci and above said paraboloid focal axis with said feed horn axis being oriented parallel to said paraboloid focal axis and intersecting said subreflector; and said focal length bearing a ratio relationship to said diameter of said main reflector that is less than one. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11)
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12. A dual offset dual reflector antenna for a V-band satellite-to-satellite communication system, said antenna comprising:
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a main reflector having a paraboloidal shape, comprising a segment of a paraboloid and defining a paraboloid focal axis, a focal length of 8.26 inches and a focal point located on said paraboloid focal axis; said main reflector having a diameter of 13 inches and subtending an arc of 68 degrees; a subreflector having a hyperboloidal shape, comprising a segment of a hyperboloid and defining first and second foci to said hyperboloidal segment; said sub-reflector being positioned with said first foci in coincident position with said focal point and said second foci being located at a predetermined position above said paraboloid focal axis and having a diameter of 3.3 inches and subtending an arc of 77 degrees; a microwave feed horn having an aperture and a feed axis; said microwave feed horn aperture being positioned at said second foci and above said focal axis with said feed horn axis being oriented parallel to said paraboloid focal axis and intersecting said subreflector; and said focal length bearing a ratio relationship to said diameter of said main reflector of 0.636.
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13. A dual offset dual reflector antenna for a satellite-to-satellite communications system, said antenna comprising:
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a main reflector having a paraboloidal shape, comprising a segment of a paraboloid and defining a paraboloid focal axis, a focal length and a focal point located on said paraboloid focal axis; said focal length bearing a ratio relationship to said diameter of said main reflector of less than one; a subreflector having a hyperboloidal shape, comprising a segment of a hyperboloid and defining first and second foci to said hyperboloidal segment; said sub-reflector being positioned with said first foci in coincident position with said focal point and said second foci being located at a predetermined position above said focal axis; and a microwave feed having a feed aperture for directing microwave energy to said subreflector, said microwave feed aperture being positioned at said second foci and above said paraboloid focal axis, and said feed having an axis oriented parallel to said paraboloid focal axis and intersecting said subreflector.
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Specification