Ka-band high-gain earth cover antenna

Patent metadata

Field	Value
Publication number	US-10476141-B2
Application number	US-201715714252-A
Country	US
Kind code	B2
Filing date	Sep 25, 2017
Priority date	Sep 25, 2017
Publication date	Nov 12, 2019
Grant date	Nov 12, 2019

Abstract

An antenna system includes a reflector, an offset feed horn and a support platform. The reflector has a reflector surface. The reflector and offset feed horn are attached to the support platform. The offset feed horn transmits RF microwave energy toward the reflector surface. The antenna system further includes a turntable which has a single rotation axis. The turntable rotates about the antenna rotation axis. The support platform is attached to the turntable such that the turntable rotates the support platform. The reflector surface has a perturbed paraboloid geometrical shape that reflects most RF microwave energy along a beam peak pointing direction. The reflector surface reflects RF microwave energy towards the earth's surface in such a manner that the reflected RF microwave energy illuminates a narrow strip of the earth's surface from nadir to a point near the earth's horizon with substantially constant intensity. The offset feed horn is oriented and positioned such that it points away from the beam peak pointing direction.

First claim

What is claimed is:

1. An antenna system comprising:
a single axis rotational turntable connected to a spacecraft by a support platform, with the turntable including means for rotating said support platform and means for providing provides increased stability as compared to conventional high gain antennas that uses a two-axis-gimbal pointing system supported by a boom;
a curved reflector attached to the support platform, the curved reflector including a reflector surface having a perturbed paraboloid geometrical shape that reflects RF microwave energy along a beam peak pointing direction, the reflector surface reflecting most of the RF microwave energy towards the earth's surface in such a manner that the reflected RF microwave energy illuminates a narrow strip of the earth's surface from nadir to a point near the earth's horizon with substantially constant intensity; and
an offset feed horn attached to the support platform to transmit RF microwave energy toward the reflector surface, the offset feed horn being oriented and positioned such that it points away from said beam peak pointing direction;
whereby the reflector surface is curved to project the illumination intensity on the earth's surface as substantially constant along a narrow strip from nadir to a point close to the horizon with a predetermined contour pattern containing a 4 dB margin along a center line of an illuminated strip with a radial coordinate representing predetermined measurement units from nadir on the earth's surface and an angular coordinate representing the azimuth angle with a substantial portion of the radiation energy emanating from the feed horn diverted towards the areas near the horizon with pattern levels drops away causing “fan-shaped” beams with one end much stronger and directed towards the horizon and the weaker end directed towards nadir;
whereby the feed horn includes a horn section and a polarizer section and further comprises two half sections removably attached together with a polarizer fin sandwiched between feed horn sections; and
the antenna system further including dual isolated waveguides, isolated to minimize energy coupling from one waveguide port to the other, whereby a first waveguide port produces right-hand circular polarization (RHCP) and a second waveguide port produces left-hand circular polarization (LHCP).

2. The antenna system according to claim 1 further comprising a support post attached to the support platform, wherein the reflector is attached to the support post.

3. The antenna system according to claim 1 further comprising a support post attached to the support platform, wherein the offset feed horn is attached to the support post.

4. The antenna system according to claim 1 wherein the offset feed horn includes a load termination device.

5. The antenna system according to claim 1 wherein the offset feed horn includes an internal waveguide and comprises a pair of feed horn sections that are connected together, each feed horn section defining a portion of the internal waveguide.

6. The antenna system according to claim 1 wherein one of the feed horn sections has a stepped recess sized for receiving the polarizer fin.

7. The antenna system according to claim 1 further comprising a feed waveguide connected to the offset feed horn to provide RF microwave energy to the feed horn.

8. The antenna system according to claim 1 wherein the reflector surface is fabricated from metal.

9. The antenna system according to claim 1 wherein the reflector is fabricated from a thermally stable, electrically conducting composite material.

Assignees

• Nasa

Inventors

• Marrero-Fontanez Victor J
• Dutoit Cornelis F

Classifications

• H01P1/171

  using a corrugated or ridged waveguide section · CPC title

• H01Q1/125

  Means for positioning · CPC title

• H01Q3/04

  for varying one co-ordinate of the orientation · CPC title

• H01Q1/288 Primary

  Satellite antennas · CPC title

• H01Q13/0258

  Orthomode horns (orthomode transducers H01P1/161) · CPC title