Deployable reflector antenna
A balloon reflector antenna for a satellite, including a spherical balloon with a surface transparent to electromagnetic waves and a reflective surface opposite the transparent surface. The balloon reflector antenna may further include a feed system extending from the center of the balloon that receives electromagnetic waves reflected off the reflective surface and/or outputs electromagnetic waves that are reflected off the reflective surface.
1. A balloon reflector antenna, comprising:
a spherical balloon with a first hemisphere comprising a transparent surface that is transparent to electromagnetic waves and a second hemisphere, opposite the first hemisphere, comprising a reflective surface having a line of focus; and
a feed system extending along one or more radial lines from a center of the spherical balloon that receives electromagnetic waves reflected off the reflective surface along the line of focus,
wherein the balloon reflector antenna is configured such that the spherical balloon and the feed system are stowable in a canister during launch of a satellite.
2. The balloon reflector antenna of claim 1 , wherein the feed system emits electromagnetic waves along the line of focus that are reflected off the reflective surface.
3. The balloon reflector antenna of claim 2 , wherein the electromagnetic waves emitted by the feed system and reflected off the reflective surface pass through the transparent surface.
4. The balloon reflector antenna of claim 1 , wherein the electromagnetic waves received by the feed system pass through the transparent surface before being reflected off the reflective surface.
5. The balloon reflector antenna of claim 1 , wherein the transparent surface has an absorption rate of less than 1 percent at a wavelength of interest.
6. The balloon reflector antenna of claim 1 , wherein the transparent surface is a flexible polymer.
7. The balloon reflector antenna of claim 1 , wherein the transparent surface is approximately 0.5 mil thick.
8. The balloon reflector antenna of claim 1 , wherein the reflective surface is formed by applying a metallic coating to the material that forms the transparent surface.
9. The balloon reflector antenna of claim 8 , wherein the metallic coating is approximately 0.5 microns thick.
10. The balloon reflector antenna of claim 1 , wherein the feed system is configured to pivot from the center of the spherical balloon to extend along any axis of the spherical balloon.
11. The balloon reflector antenna of claim 1 , wherein the balloon reflector antenna is configured to transmit images captured by a satellite imaging system.
12. The balloon reflector antenna of claim 1 , wherein the balloon reflector antenna is configured to transmit images captured by a second balloon reflector antenna via synthetic aperture radar.
13. The balloon reflector antenna of claim 1 , wherein the balloon reflector antenna is configured to retransmit a signal received by a second balloon reflector antenna.
14. The balloon reflector antenna of claim 1 , further comprising:
at least one dielectric support curtain along a diameter of the spherical balloon.
15. The balloon reflector antenna of claim 1 , wherein the canister is one or more CubeSat units.
16. The balloon reflector antenna of claim 1 , wherein the balloon reflector antenna is configured such that the spherical balloon is inflatable.
17. The balloon reflector antenna of claim 16 , wherein the balloon reflector antenna is configured such that the feed system is pulled out of the canister when the spherical balloon is inflating or inflated.
18. A method of making a balloon reflector antenna, the method comprising:
providing a spherical balloon with a first hemisphere comprising a transparent surface that is transparent to electromagnetic waves and a second hemisphere, opposite the first hemisphere, comprising a reflective surface having a line of focus;
providing a feed system extending along one or more radial lines from the center of the balloon that receives electromagnetic waves reflected off the reflective surface along the line of focus;
stowing the spherical balloon, in an uninflated state, in a canister;
stowing the feed system in the canister;
launching a satellite that includes the canister into space;
inflating the spherical balloon while the satellite is in orbit, and
pulling the feed system, while the satellite is in orbit, out of the canister into the inflating or inflated spherical balloon.
19. The method of claim 18 , wherein the feed system emits electromagnetic waves along the line of focus that are reflected off the reflective surface.
20. The method of claim 18 , wherein the canister is one or more CubeSat units.
21. The balloon reflector antenna of claim 1 , wherein:
the transparent surface of the first hemisphere is continuous throughout the first hemisphere; and
the reflective surface of the second hemisphere is continuous throughout the second hemisphere.
22. The method of claim 18 , wherein the electromagnetic waves received by the feed system pass through the transparent surface before being reflected off the reflective surface.
23. The method of claim 19 , wherein the spherical balloon is configured such that the electromagnetic waves that are reflected off the reflective surface pass through the transparent surface.