Space based local area network (SBLAN)

1. A space based local area network system for providing dynamically allocated downlink services for spacecraft in Geosynchronous Earth Orbit, the system comprising:

at least two client satellites which host an inter-satellite communications payload and which are in communication only with other satellites;

a hub satellite which hosts an inter-satellite communications payload, a downlink communications payload, and an aggregator payload; and

a ground station which transmits data to and receives data from the hub satellite,

wherein the hub satellite, using the aggregator payload, aggregates at least two data flows received from the at least two client satellites over an inter-satellite link, by the inter-satellite communications payload, into a data stream that is downlinked to the ground station, using the downlink communications payload, over a space-to-ground link.

2. The space based local area network system according to claim 1 , wherein the ground station includes a space based local area network kit comprising:

a gateway router; and

a software defined radio,

wherein the gateway router routes data through the software defined radio which transmits data to and receives data from the hub satellite over the space-to-ground link.

3. The space based local area network system according to claim 1 , wherein the hub satellite is a switched digital hub which includes a space based local area networking kit comprising:

a software defined radio; and

an Internet protocol router,

wherein signals received at the hub satellite are demodulated and packets are routed, and

wherein packet data is remodulated onto the space-to-ground link or an inter-satellite link.

4. The space based local area network system according to claim 3 , wherein the software defined radio hosts the Internet protocol router.

5. The space based local area network system according to claim 3 , wherein the Internet protocol router is separate from the software defined radio.

6. The space based local area network system according to claim 1 , wherein the hub satellite is a bent pipe hub which includes a space based local area networking kit comprising a radio frequency switching network.

7. The space based local area network system according to claim 6 , wherein the radio frequency switching network comprises:

first dedicated uplink and first dedicated downlink RF channels for the space-to-ground link;

second dedicated uplink and second dedicated downlink Ka-band channels for hub-to-client links.

8. The space based local area network system according to claim 7 , wherein the radio frequency switching network further comprises Ka-to-Ka band translation for communication between client satellites.

9. The space based local area network system according to claim 1 , wherein the at least two client satellites includes a space based local area network kit comprising:

a software defined radio; and

an Internet protocol router.

10. The space based local area network system according to claim 9 , wherein the software defined radio hosts the Internet protocol router.

11. The space based local area network system according to claim 9 , wherein the Internet protocol router is separate from the software defined radio.

12. The space based local area network system according to claim 1 , wherein a frequency band around 22.5 GHz is used for data transfer over the inter-satellite link between the at least two client satellites and the hub satellite.

13. The space based local area network system according to claim 1 , wherein the inter-satellite link uses an 802.16 physical layer.

14. The space based local area network system according to claim 13 , wherein the 802.16 physical layer uses 8PSK modulation and a low density parity check coding scheme.

15. The space based local area network system according to claim 1 , wherein the hub satellite further comprises a sector beam antenna, and the at least two client satellites further comprise a steerable spot beam antenna.

16. The space based local area network system according to claim 1 , wherein the at least two client satellites are positioned within 300 km of the hub satellite.

17. The space based local area network system according to claim 3 , wherein the software defined radio comprises:

a first IF/RF digital slice; and

a second IF/RF digital slice,

wherein the first IF/RF digital slice and the second IF/RF digital slice each comprise an integrated package of multiple field programmable gate arrays, application specific integrated circuits, high-speed memory, and I/O ports.

18. The space based local area network system according to claim 17 ,

wherein the first IR/RF digital slice is a Ka-band IF/RF digital slice and the second IF/RF digital slice is a C-band IF/RF digital slice,

wherein the first IF/RF digital slice includes software or firmware for performing Ka-band signal transmission, and

wherein the second IF/RF digital slice includes software or firmware for performing C-band signal transmission.

19. The space based local area network system according to claim 9 , wherein the software defined radio comprises a Ka-band IF/RF digital slice,

wherein the Ka-band IF/RF digital slice comprises an integrated package of multiple field programmable gate arrays, application specific integrated circuits, high-speed memory, and I/O ports, and

wherein the Ka-band IF/RF digital slice includes software or firmware for performing Ka-band signal transmission.

20. A space based local area networking kit for a hub satellite which provides dynamically allocated downlink services for spacecraft in Geosynchronous Earth Orbit, the space based local area networking kit comprising:

a software defined radio; and

an Internet protocol router,

wherein the hub satellite is in communication only with other satellites, and

wherein the software defined radio and the Internet protocol router are configured to demodulate signals received at the hub satellite from at least two client satellites over an inter-satellite link or a ground station over a space-to-ground link, route packets, and remodulate packet data onto one of the inter-satellite link and the space-to-ground link.

21. A method for providing dynamically allocated downlink services for spacecraft in Geosynchronous Earth Orbit, the method comprising:

receiving, at a hub satellite, data transmitted over an inter-satellite link from at least two client satellites that are in communication only with other satellites;

aggregating the data transmitted over the inter-satellite link from the at least two client satellites; and

transmitting the aggregated data from the hub satellite to a ground station over a space-to-ground link.

22. The method of claim 21 , wherein the inter-satellite link and the RF space-to ground link use at least one of C-band channels, Ku-band channels, Ka-band channels, S-band channels, or X-band channels.

23. The method of claim 21 , wherein a frequency band around 22.5 GHz is used for data transfer over the inter-satellite link between the at least two client satellites and the hub satellite.

24. The method of claim 21 , wherein the inter-satellite link uses an 802.16 physical layer.

25. The method of claim 24 , wherein the 802.16 physical layer uses 8PSK modulation and a low density parity check coding scheme.