Satellite data communication system and method

1. A satellite communication system being configured and operable to operate in one or more frequency bands to simultaneously relay data signals between a plurality of remote terminals and one or more ground stations (gateways) in both return and forward links, the satellite communication system comprising a processor configured and operable to receive from each of said remote terminals an uplink return signal in the form of a plurality of terminal return signals spread over a predetermined first frequency allocation in said one or more frequency bands according to a predetermined spread function, de-spread the received plurality of terminal return signals, and generate a downlink return signal, corresponding to at least some of the received plurality of spread terminal return signals and having a predetermined second frequency allocation, to be sent to one of the ground stations, wherein said processor is further configured and operable to receive from one of the ground stations an uplink forward signal having a predetermined third frequency allocation, spread the uplink forward signal into a plurality of gateway forward signals spread over at least part of said predetermined first frequency allocation according to a predetermined second spread function, and generate a corresponding plurality of downlink forward signals to be sent to and received by the remote terminal.

2. The satellite communication system according to claim 1 , wherein a bandwidth of said second frequency allocation is narrower than a sum of bandwidths of said at least some of the spread terminal return signals.

3. The satellite communication system according to claim 2 , wherein said processor is configured and operable to receive from the ground station said uplink forward signal and spread the uplink forward signal into the plurality of gateway forward signals, wherein spreading factor of said second spread function ranges between 10 and 50.

4. The satellite communication system according to claim 3 , wherein accumulative bandwidth of said downlink return signals is in a range of tens of MHz to several GHz.

5. The satellite communication system according to claim 1 being configured and operable to operate in one or more of the following frequency bands: Ka, Q, V and W.

6. The satellite communication system according to claim 1 , comprising an un-furlable reflector antenna for receiving said plurality of terminal return signals.

7. The satellite communication system according to claim 1 , comprising an antenna having a phased-array feeding network.

8. The satellite communication system according to claim 1 having a high G/T thereby minimizing power and footprint of the remote terminal.

9. The satellite communication system according to claim 1 , wherein said spread function is of a higher de-spreading factor than spreading factor of said second spread function.

10. The satellite communication system according to claim 1 , wherein said processor is configured and operable to receive said plurality of terminal return signals and de-spread them into said single uplink return signal, wherein de-spreading factor of said spread function ranges between 100 and 500.

11. The satellite communication system according to claim 1 , being configured and operable to simultaneously receive and process uplink return signals from at least 200 remote terminals.

12. The satellite communication system according to claim 1 , wherein the bandwidth of said first frequency allocation is in a range of tens of MHz to hundreds of MHz.

13. A satellite for use in space-based communication, comprising the satellite communication system of claim 1 .

14. The satellite according to claim 13 , being a geostationary satellite.

15. The remote terminal according to claim 14 , wherein at least one of the following:

the remote terminal comprises an array of radiating elements configured and operable to generate said plurality of terminal return signals;

the remote terminal having a size of a few centimeters.

16. A remote terminal for use with the satellite communication system of claim 1 .

17. A method for space-based internet data communication, comprising:

spreading a return signal, at uplink portion of a return channel, into a plurality of terminal return signals over a predetermined first frequency allocation according to a predetermined spreading factor; and

de-spreading the terminal return signals to reconstruct said return signal and sending the return signal through downlink portion of the return channel at a predetermined second frequency allocation a bandwidth of which being less than a bandwidth of said first frequency allocation by a predetermined ratio,

receiving from one of the ground stations an uplink forward signal having a predetermined third frequency allocation,

spreading the uplink forward signal into a plurality of gateway forward signals spread over at least part of said predetermined first frequency allocation according to a predetermined second spread function, and

generating a corresponding plurality of downlink forward signals to be sent to and received by the remote terminal.

18. The method according to claim 17 , further comprising spreading a forward signal, at downlink portion of a forward channel, into a plurality of gateway forward signals over a predetermined third frequency allocation according to a predetermined second spreading factor.

19. The method according to claim 17 , wherein at least one of the following:

said spreading factor is between 100 and 500;

said second spreading factor is between 10 and 50.