Cross-link satellite with spherical reflectors
US-10938117-B2 · Mar 2, 2021 · US
US11414217B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11414217-B2 |
| Application number | US-202016743264-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jan 15, 2020 |
| Priority date | Jan 15, 2020 |
| Publication date | Aug 16, 2022 |
| Grant date | Aug 16, 2022 |
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A large reflector inflatable telescope. The telescope has an inflatable hull with a conical lower portion and a hemispherical upper portion. The conical portion is transparent to electromagnetic waves so that radio or light waves can reach an inner reflector, which is interposed between the conical portion and the hemispherical portion. The presence of the inner reflector allows the conical portion and the hemispherical portion to be inflated at different pressures such that the reflector becomes spherical or parabolic. If desired, the reflector can be made adjustable with a membrane behind the reflector that provides electro-static force to shape the reflector.
Opening claim text (preview).
What is claimed is: 1. A large reflector inflatable telescope, comprising: an inflatable hull, made from flexible film and having a generally conical lower portion and a generally hemispherical upper portion; wherein the conical portion is transparent to electromagnetic waves; an inner reflector, made from a flexible film and interposed between the conical portion and the hemispherical portion, thereby making the conical portion and the hemispherical portion inflatable at different pressures such that the reflector becomes spherical or parabolic; and wherein the reflector is reflective on a surface of the reflector facing into the conical portion. 2. The telescope of claim 1 , further comprising an inflation system, operable to separately inflate the conical portion and the hemispherical portion to two different pressures, with the pressure of the conical portion being greater than the pressure of the hemispherical portion. 3. The telescope of claim 2 , wherein the inflation system has a means for providing pressurized gas. 4. The telescope of claim 1 , further comprising at least one sun shield layer within the hemispherical portion above the reflector, and made from a thin metalized film. 5. The telescope of claim 1 , wherein the hull and reflector are foldable and stowable in launch vehicle. 6. The telescope of claim 1 , wherein the reflector is reflective due to a reflective coating applied to a surface of the reflector. 7. The telescope of claim 1 , further comprising a membrane separating the conical portion of the hull into an upper conical portion and a lower conical portion. 8. The telescope of claim 7 , wherein the inflation system is operable to inflate the lower conical portion to a pressure higher than the pressure of the upper conical portion. 9. The telescope of claim 1 , further comprising a receiver that receives electromagnetic waves reflected from the reflector and/or transmits electromagnetic waves to be reflected off the reflector. 10. A large reflector inflatable telescope having an adjustable reflector, comprising: an inflatable hull, made from flexible film and having a generally conical lower portion and a generally hemispherical upper portion; wherein the conical portion is transparent to electromagnetic waves; an inner reflector, made from a flexible film and interposed between the conical portion and the hemispherical portion, thereby making the conical portion and the hemispherical portion inflatable at different pressures such that the reflector becomes spherical or parabolic; and wherein the reflector is reflective on a surface of the reflector facing into the conical portion, and is electrically conductive; a flexible membrane within the hemispherical hull portion and spaced from the reflector to form a compartment behind the reflector; an electrode grid covering the surface of the membrane; and a reflector adjustment controller operable to electrically activate electrodes of the electrode grid. 11. The telescope of claim 10 , further comprising an inflation system, operable to separately inflate the conical portion and the hemispherical portion to two different pressures, with the pressure of the conical portion being greater than the pressure of the hemispherical portion. 12. The telescope of claim 11 , wherein the inflation system has a means for providing pressurized gas. 13. The telescope of claim 10 , further comprising at least one sun shield layer within the hemispherical portion above the reflector and made from a thin metalized film. 14. The telescope of claim 10 , wherein the hull, reflector, and membrane are foldable and stowable in launch vehicle. 15. The telescope of claim 10 , wherein the reflector is reflective due to a reflective coating applied to a surface of the reflector. 16. The telescope of claim 10 , further comprising a membrane separating the conical portion of the hull into an upper conical portion and a lower conical portion. 17. The telescope of claim 16 , wherein the inflation system is operable to inflate the lower conical portion to a pressure higher than the pressure of the upper conical portion. 18. The telescope of claim 10 , further comprising a receiver that receives electromagnetic waves reflected from the reflector and/or transmits electromagnetic waves to be reflected off the reflector. 19. The telescope of claim 10 , wherein the controller is operable to activate each electrode individually. 20. The telescope of claim 10 , further comprising sensors operable to determine a curvature of the reflector, and to deliver data representing the curvature to the controller.
involving prisms or mirrors (G02B23/14 takes precedence) · CPC title
Mountings or tracking · CPC title
Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles · CPC title
the reflecting element being a flexible sheet or membrane, e.g. for varying the focus (flexible mirrors for cosmetic use A45D42/24) · CPC title
at least one surface having optical power · CPC title
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