Low earth orbit satellite constellation system
In some embodiments, a communications system can include a plurality of low earth orbit (LEO) satellites deployed at different altitudes and configured to communicate with one or more terrestrial devices and with one another. The communications system may further include a plurality of geosynchronous (GEO) satellites deployed above the plurality of LEO satellites. The plurality of LEO satellites may cooperate with one another and with the plurality of GEO satellites to provide a global communication network having redundant point-to-point communication.
1 . A communications system comprising:
at least one modular satellite, each modular satellite including:
a spacecraft bus;
a pair of solar wings coupled to the spacecraft bus and configured to extend and retract, and further configured to generate electricity from received light;
a plurality of electrical interconnects; and
a pair of phased array antennas coupled to the spacecraft bus and communicatively coupled by the plurality of electrical interconnects, the pair of phased array antennas including a plurality of tiles, wherein one or more of the plurality of tiles is connected to one or more neighboring tiles by one or more articulating joints, each tile including circuitry including an embedded processing circuit configured to provide channelization and packet processing functionality.
2 . The communications system of claim 1 , wherein each modular satellite is configured to determine a communication path through a constellation of satellites including the at least one modular satellite to provide a point-to-point communication path avoiding multiple ground hops.
3 . The communications system of claim 1 , wherein the at least one modular satellite further includes a plurality of satellites.
4 . The communications system of claim 3 , wherein the plurality of satellites includes:
a plurality of low earth orbit (LEO) satellites deployed at different altitudes and configured to communicate with one or more terrestrial devices and with one another at selected band frequencies;
a plurality of geosynchronous (GEO) satellites deployed above the plurality of LEO satellites, each GEO satellite configured to operate at V or other frequency Bands such that a power flux density of one or more geostationary orbit (GSO) satellites is not interfered; and
wherein the plurality of LEO satellites cooperate with one another and with the plurality of GEO satellites to provide a global communication having redundant point-to-point communication.
5 . The communications system of claim 1 , further including a communication device including at least two receivers configured to receive signals at frequencies greater than 10 GHz and at least two transmitters configured to send signals at frequencies greater than 10 GHz, the communication device configured to communicate with the at least one modular satellite.
6 . The communications system of claim 5 , wherein the communication device receives at 20 GHz and transmits at 30 GHz.
7 . The communications system of claim 5 , wherein the at least two receivers and the at least two transmitters are integrated within the communication device.
8 . The communications system of claim 5 , wherein the communication device transmits data packets including at least two identifiers corresponding to two different LEO satellites of a plurality of LEO satellites.
9 . The communications system of claim 8 , wherein, when a GEO satellite is in view, the communications device transmits the data packets including at least one identifier corresponding to the GEO satellite.
10 . The communications system of claim 1 , wherein each of the phased array antennas is configured to be mechanically and electronically articulated to limit equivalent power flux density interference when in direct view of a GEO satellite associated with another operator.