Satellite system that produces optical inter-satellite link (ISL) beam based on optical ISL received from another satellite
Described herein is a space based subsystem of a satellite, and methods for use therewith, for receiving an optical ISL beam from another satellite, and in dependence therein, producing a further optical ISL beam for transmission to a further satellite. Additionally, the subsystem can also produce RF service downlink beams for transmission to service terminals. The subsystem can include, inter alia, receiver optics, optical amplifiers, a WDM demultiplexer, beam splitters, a WDM multiplexer, and transmitter optics. In certain embodiments, because RF frequencies of a wavelength division multiplexed optical signal produced by the WDM multiplexer are within a same specified RF frequency range within which the satellite and the further satellite are configured to transmit RF service downlink beams, there is an elimination of any need for the satellite and further satellite to perform any frequency conversions when producing the RF service downlink beams in dependence on the optical ISL beams.
1. A space based subsystem of a satellite, the space based subsystem comprising:
receiver optics configured to receive an optical inter-satellite (ISL) beam from another satellite and output an optical ISL signal;
a first optical amplifier optically coupled to the receiver optics and configured to amplify the optical ISL signal that is output from the receiver optics;
a wavelength-division multiplexing (WDM) demultiplexer optically coupled to the first optical amplifier and configured to demultiplex and thereby separate the amplified optical ISL signal, which is output from the first optical amplifier, into a plurality of separate optical signals that each have a different peak wavelength within a specified optical wavelength range;
a plurality of beam splitters, each of which is configured to split a respective one of at least a subset of the separate optical signals that are output from the WDM demultiplexer into a respective pair of optical signals, the plurality of beam splitters thereby collectively configured to produce a plurality of separate pairs of optical signals that each have a different peak wavelength within the specified optical wavelength range, with the optical signals of a same pair having the same peak wavelength;
a WDM multiplexer configured to receive one of the optical signals of each of the separate pairs of optical signals, and thereby receive a plurality of optical signals that each have a different peak wavelength within the specified optical wavelength range, and configured to multiplex and thereby combine the received optical signals onto a single optical fiber on which each of the optical signals are carried at a same time on its own separate optical wavelength within the specified optical wavelength range as a wavelength division multiplexed optical signal;
a second optical amplifier optically coupled to the single optical fiber and configured to amplify the wavelength division multiplexed optical signal that is output by the WDM multiplexer; and
transmitter optics configured to receive the amplified wavelength division multiplexed optical signal and, in dependence therein, transmit a further optical inter-satellite link (ISL) beam to a further satellite.
2. The subsystem of claim 1 , wherein because RF frequencies of the wavelength division multiplexed optical signal are within a same specified RF frequency range within which the further satellite is configured to transmit a plurality of RF service downlink beams, there is an elimination of any need for the further satellite to perform any frequency conversions when producing the plurality of RF service downlink beams in dependence on the further optical ISL beam.
3. The subsystem of claim 1 , further comprising filters within signal paths between the beam splitters and the WDM multiplexer.
4. The subsystem of claim 1 , wherein the specified optical wavelength range is either a contiguous, or a non-contiguous, optical wavelength range within an infrared (IR) spectrum.
5. The subsystem of claim 1 , further comprising:
a plurality of photodetectors, each of which is configured to receive the other one of the optical signals of each of the separate pairs of optical signals produced by the beam splitters, and thereby collectively receive a plurality of optical signals that each have a different peak wavelength within the specified frequency range, and each of the photodetectors configured to convert a different one of the optical signals to a respective electrical data signal having an RF frequency within a same specified RF frequency range within which the space based subsystem is configured to transmit a plurality of RF service downlink beams; and
one or more RF components and antennas configured to produce and transmit, in dependence on the electrical data signals generated by the plurality of PDs, the plurality of RF service downlink beams within the specified RF frequency range;
wherein because the RF frequencies of the electrical data signals output by the photodetectors are within the same specified RF frequency range within which the space based subsystem is configured to transmit the plurality of RF service downlink beams, there is an elimination of any need for the space based subsystem of the satellite to perform any frequency conversions when producing the plurality of RF service downlink beams in dependence on the optical ISL beam.
6. The subsystem of claim 5 , further comprising filters within signal paths between the beam splitters and the photodetectors.
7. The subsystem of claim 5 , wherein the specified optical wavelength range is either a contiguous, or a non-contiguous, optical wavelength range within an infrared (IR) spectrum.
8. The subsystem of claim 5 , wherein the specified RF frequency range within which the satellite is configured to produce and transmit a plurality of RF service downlink beams comprises a downlink portion of the Ka band.
9. The subsystem of claim 8 , wherein the downlink portion of the Ka band is from 17.7 GHz to 20.2 GHz, and thus, has a bandwidth of 2.5 GHz.
10. The subsystem of claim 8 , wherein the downlink portion of the Ka band is from 17.3 GHz to 20.2 GHz, and thus, has a bandwidth of 2.9 GHz.
11. A space based subsystem of a satellite, the space based subsystem comprising:
receiver optics configured to receive an optical inter-satellite (ISL) beam from another satellite and output an optical ISL signal;
a first optical amplifier optically coupled to the receiver optics and configured to amplify the optical ISL signal that is output from the receiver optics;
a wavelength-division multiplexing (WDM) demultiplexer optically coupled to the first optical amplifier and configured to demultiplex and thereby separate the amplified optical ISL signal, which is output from the optical amplifier, into a plurality of separate optical signals that each have a different peak wavelength within a specified optical wavelength range;
a WDM multiplexer configured to receive a subset of the optical signals that each have a different peak wavelength within the specified optical wavelength range, and configured to multiplex and thereby combine the received subset of the optical signals onto a single optical fiber on which each of the optical signals are carried at a same time on its own separate optical wavelength within the specified optical wavelength range as a wavelength division multiplexed optical signal;
a second optical amplifier optically coupled to the single optical fiber and configured to amplify the wavelength divisional multiplexed optical signal that is output by the WDM multiplexer;
transmitter optics configured to receive the amplified wavelength divisional multiplexed optical signal and, in dependence therein, transmit a further optical inter-satellite link (ISL) beam to a further satellite;
a plurality of photodetectors, each of which is configured to receive one of a further subset of the optical signals that each have a different peak wavelength within the specified optical wavelength range, and thereby collectively receive the further subset of the optical signals that each have a different peak wavelength within the specified frequency range, and each of the photodetectors configured to convert a different one of the optical signals in the further subset to a respective electrical data signal having an RF frequency within a same specified RF frequency range within which the space based subsystem is configured to transmit a plurality of RF service downlink beams; and
one or more RF components and antennas configured to produce and transmit, in dependence on the electrical data signals generated by the plurality of PDs, the plurality of RF service downlink beams within the specified RF frequency range.
12. The subsystem of claim 11 , wherein because RF frequencies of the wavelength division multiplexed optical signal are within a same specified RF frequency range within which the further satellite is configured to transmit a plurality of RF service downlink beams, there is an elimination of any need for the further satellite to perform any frequency conversions when producing the plurality of RF service downlink beams in dependence on the further optical ISL beam.
13. The subsystem of claim 11 , further comprising filters within signal paths between the WDM demultiplexer and the WDM multiplexer.
14. The subsystem of claim 11 , wherein the specified optical wavelength range is either a contiguous, or a non-contiguous, optical wavelength range within an infrared (IR) spectrum.
15. The subsystem of claim 11 , wherein because the RF frequencies of the electrical data signals output by the photodetectors are within the same specified RF frequency range within which the space based subsystem is configured to transmit the plurality of RF service downlink beams, there is an elimination of any need for the space based subsystem to perform any frequency conversions when producing the plurality of RF service downlink beams in dependence on the optical ISL beam received from the other satellite.
16. The subsystem of claim 15 , wherein the specified RF frequency range within which the satellite is configured to produce and transmit a plurality of RF service downlink beams comprises a downlink portion of the Ka band.
17. The subsystem of claim 16 , wherein the downlink portion of the Ka band is from 17.7 GHz to 20.2 GHz, and thus, has a bandwidth of 2.5 GHz.
18. The subsystem of claim 16 , wherein the downlink portion of the Ka band is from 17.3 GHz to 20.2 GHz, and thus, has a bandwidth of 2.9 GHz.
19. The subsystem of claim 11 , further comprising filters within signal paths between the WDM demultiplexer and the photodetectors.
20. The subsystem of claim 11 , wherein the specified optical wavelength range is either a contiguous, or a non-contiguous, optical wavelength range within an infrared (IR) spectrum.
21. A method for use by a space based subsystem, the method comprising:
receiving an optical inter-satellite link (ISL) beam from another satellite;
producing, in dependence on the received optical ISL beam, a plurality of separate optical signals that each have a different peak wavelength within a specified optical wavelength range;
splitting at least a subset of the separate optical signals into a respective pair of optical signals, and thereby producing separate pairs of optical signals that each have a different peak wavelength within the specified optical wavelength range, with the optical signals of a same pair having the same peak wavelength;
multiplexing a plurality of the optical signals that each have a different peak wavelength within the specified optical wavelength range, the optical signals being multiplexed including one of the optical signals of each of the separate pairs of optical signals, to thereby produce a wavelength division multiplexed optical signal that includes data that is to be forwarded to another satellite so that the other satellite can transmit, in dependence thereon, a plurality of RF service downlink beams;
producing a further optical inter-satellite link (ISL) beam in dependence on the wavelength division multiplexed optical signal; and
transmitting the further optical ISL beam through free-space to a further satellite;
wherein because RF frequencies of the wavelength division multiplexed optical signal are within the same specified RF frequency range within which the further satellite is configured to transmit the plurality of RF service downlink beams, there is an elimination of any need for the further satellite to perform any frequency conversions when producing the plurality of RF service downlink beams in dependence on the optical ISL beam.
22. The method of claim 21 , further comprising:
converting each of optical signals, that each have a different peak wavelength within the specified optical wavelength range, into a respective electrical data signal having an RF frequency within the same specified RF frequency range within which the space based subsystem is configured to transmit a plurality of RF service downlink beams, the optical signals being converted including the other one of the optical signals of each of the separate pairs of optical signals;
producing, in dependence on the electrical data signals, the plurality of RF service downlink beams within the specified RF frequency range; and
transmitting the plurality of RF service downlink beams within the specified RF frequency range;
wherein because the RF frequencies of the electrical data signals resulting from the converting are within the same specified RF frequency range within which the space based subsystem is configured to transmit the plurality of RF service downlink beams, there is an elimination of any need for the space based subsystem to perform any frequency conversions when producing the plurality of RF service downlink beams in dependence on the optical ISL uplink beam.
23. The method of claim 22 , wherein the specified RF frequency range within which the satellite and the other satellite are configured to produce and transmit a plurality of RF service downlink beams comprises a downlink portion of the Ka band.
24. The method of claim 23 , wherein:
the downlink portion of the Ka band is from 17.7 GHz to 20.2 GHz, and thus, has a bandwidth of 2.5 GHz; or
the downlink portion of the Ka band is from 17.3 GHz to 20.2 GHz, and thus, has a bandwidth of 2.9 GHz.
25. The method of claim 21 , wherein the specified optical wavelength range is either a contiguous, or a non-contiguous, optical wavelength range within an infrared (IR) spectrum.
26. A method for use by a space based subsystem of a satellite, the method comprising:
receiving an optical inter-satellite link (ISL) beam from another satellite;
producing, in dependence on the received optical ISL beam, a plurality of separate optical signals that each have a different peak wavelength within a specified optical wavelength range;
multiplexing a first subset of the optical signals that each have a different peak wavelength within the specified optical wavelength range to thereby produce a wavelength division multiplexed optical signal that includes data that is to be forwarded to a further satellite so that the further satellite can transmit, in dependence thereon, a plurality of RF service downlink beams;
producing an optical inter-satellite link (ISL) beam, in dependence on the wavelength division multiplexed optical signal;
transmitting the optical ISL beam through free-space to the further satellite;
converting each of a second subset of the optical signals, that each have a different peak wavelength within the specified optical wavelength range, into a respective electrical data signal having an RF frequency within the same specified RF frequency range within which the space based subsystem is configured to transmit a plurality of RF service downlink beams;
producing, in dependence on the electrical data signals, the plurality of RF service downlink beams within the specified RF frequency range; and
transmitting the plurality of RF service downlink beams within the specified RF frequency range.
27. The method of claim 26 , wherein:
because RF frequencies of the wavelength division multiplexed optical signal are within the same specified RF frequency range within which the further satellite is configured to transmit the plurality of RF service downlink beams, there is an elimination of any need for the further satellite to perform any frequency conversions when producing the plurality of RF service downlink beams in dependence on the optical ISL beam; and
because the RF frequencies of the electrical data signals resulting from the converting are within the same specified RF frequency range within which the space based subsystem is configured to transmit the plurality of RF service downlink beams, there is an elimination of any need for the space based subsystem to perform any frequency conversions when producing the plurality of RF service downlink beams in dependence on the optical ISL beam.
28. The method of claim 27 , wherein the specified RF frequency range within which the satellite and the other satellite are configured to produce and transmit a plurality of RF service downlink beams comprises a downlink portion of the Ka band.
29. The method of claim 28 , wherein:
the downlink portion of the Ka band is from 17.7 GHz to 20.2 GHz, and thus, has a bandwidth of 2.5 GHz; or
the downlink portion of the Ka band is from 17.3 GHz to 20.2 GHz, and thus, has a bandwidth of 2.9 GHz.
30. The method of claim 26 , wherein the specified optical wavelength range is either a contiguous, or a non-contiguous, optical wavelength range within an infrared (IR) spectrum.