IP Library Granted Patent US 11,581,663
Granted Patent B1
US 11,581,663 · App. 17/319,195 · Granted Feb 14, 2023

Shaped reflector dual S-band and Ka-band high gain antenna

Inventors: Victor Marrero Fontanez (Greenbelt, MD); Cornelis Du Toit (Ellicott City, MD); Aaron Dabrowski (Arlington, VA)
Assignee: United States of America as represented by the Administrator of NASA
H01Q21/30H01Q9/0478H01Q15/0013
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Quick Facts
Patent No.
US 11,581,663
App. No.
17/319,195
Granted
Feb 14, 2023
Kind
B1
Abstract

An apparatus for space and terrestrial communication applications includes a Ka-band horn combined with a S-band cross-polarization cup. The S-band cross-polarization cup is placed around a neck of the Ka-band horn in a form of a collar.

Claims (24)

1. An antenna for use in space and terrestrial communication applications, comprising:

a Ka-band horn with an outer circular wall with a predetermined diameter combined with a S-band cross-polarization cup, wherein

the S-band cross-polarization cup is placed around a neck of the Ka-band horn in a form of a collar, whereby said collar includes a circumferential choke slot in a cylindrical side of the Ka-band horn resulting in a constant antenna footprint and increased beam width with a reduced outer circular wall diameter.

2. The apparatus of claim 1 , wherein the Ka-band feed horn is configured to illuminate a frequency selective surface (FSS), the FSS being highly reflective, and

the highly reflective FSS is configured to illuminate a primary reflector, producing a coherent, narrow Ka-band beam.

3. The apparatus of claim 1 , wherein the Ka-band feed horn improves on a standard Potter horn with significant lower sidelobe and cross-polarization level performance by employing a modified smooth S-curved interior profile.

4. The apparatus of claim 1 , wherein the S-band cross-polarization cup is configured to reduce a cross-polarization in the S-band by cancelling reflections back to a S-band feed antenna that reflects off a central part of the reflector, the Ka-band horn and a support structure of the reflector.

5. A high gain dual S- and Ka-band circularly polarized antenna (“antenna”) for space and terrestrial communications, the antenna comprising:

a primary reflector and a secondary reflector designed and shaped for optimal Ka-band gain while a frequency selective surface on the secondary reflector provides reflectivity at Ka-band, wherein

the primary reflector is a Cassegrain-based Ka-band reflector with an outer circular wall with a predetermined diameter, and

the secondary reflector is a Ka-band reflector combined with a S-band cross-polarization cup, wherein

the S-band cross-polarization cup is placed around a neck of the Ka-band horn in a form of a collar, whereby said collar includes a circumferential choke slot in a cylindrical side of the Ka-band horn resulting in a constant antenna footprint and increased beam width with a reduced outer circular wall diameter.

6. The antenna of claim 5 , wherein the secondary reflector and the frequency selective surface may is configured to act as a dielectric radome for a S-band feed antenna.

7. The antenna of claim 5 , wherein the second reflector and the frequency selective surface are supported by struts, positioning a S-band feed phase center at the primary reflector focus.

8. The antenna of claim 7 , wherein the struts supporting the second reflector and the frequency selective surface force the frequency selective surface to act as a secondary reflector for the antenna.

9. The antenna of claim 5 , further comprising:

a Ka-band feed horn phase center is positioned at a Ka-band secondary focal point.

10. The antenna of claim 5 , wherein the primary reflector is configured to illuminate the frequency selective surface.

11. The antenna of claim 10 , wherein the illumination causes a reflection from frequency selective surface or the secondary reflector illuminating the primary reflector, thereby producing a coherent, narrow Ka-band beam.

12. The antenna of claim 5 , wherein the primary reflector and secondary reflector are shaped to provide an aperture wavefront of uniform phase and amplitude, for optimal aperture efficiency.

13. The antenna of claim 5 , wherein a shape of the secondary reflector diverts radiation energy away from a central part of the primary reflector.

14. The antenna of claim 5 , wherein the secondary reflector comprises a S-band cross-polarization cup configured to reduce antenna cross-polarization in the S-band.

15. The antenna of claim 14 , wherein the reduction of the antenna cross-polarization in the S-band is achieved by cancelling reflections back to a S-band feed antenna that reflects off a central part of the secondary reflector, the primary reflector and support structures.

16. The antenna of claim 5 , wherein a curvature, and a lip along an edge, of the cup increases a stiffness compared to a flat annular disk with a same diameter and mass.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 13, 2022
From: MARRERO FONTANEZ, VICTOR
To: UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF NASA
Reel/Frame 058648/0485 →
Continuity (1)
Provisional Application 63074190 · Sep 3, 2020