Broadband satellite payload architecture

1. A spacecraft comprising:

a payload subsystem, the payload subsystem including

a phased array of feed elements configured to illuminate an antenna reflector;

a beam forming network (BFN) coupled with the array of feed elements; and

a plurality of power amplifiers disposed between the BFN and the array of feed elements, wherein:

the phased array of feed elements forms a plurality of beams, each beam being formed by a center feed element, and a plurality of edge feed elements surrounding the center feed element;

the BFN includes a plurality of variable amplitude and phase (VAP) adjusting arrangements disposed between (i) m:1 power combiners that are communicatively coupled with the power amplifiers and (ii) at least one 1:n power splitter;

each VAP adjusting arrangement is communicatively coupled with a single respective one of the feed elements, and at least some of the feed elements are coupled with multiple VAP adjusting arrangements such that the payload subsystem includes more VAP adjusting arrangements than feed elements;

each center feed element is communicatively coupled by way of a single respective VAP adjusting arrangement with a single respective power 1:n power splitter and at least some edge feed elements are communicatively coupled by way of respective ones of the m:1 power combiners with two or more 1:n power splitters; and

m is greater than 1, and n is greater than 2.

2. The spacecraft of claim 1 , wherein the spacecraft is configured to receive a ground command and beamforming coefficients of one or more of the VAP adjusting arrangements are correctable by the ground command.

3. The spacecraft of claim 2 , wherein a failure of one or more of the power amplifiers is compensatable by correcting, by the ground command, the beamforming coefficients of one or more of the VAP adjusting arrangements.

4. The spacecraft of claim 1 , wherein the plurality of power amplifiers are coupled with the array of feed elements.

5. The spacecraft of claim 1 , wherein the plurality of feed elements consists of six edge feed elements disposed adjacent to and surrounding the center feed element.

6. The spacecraft of claim 5 , wherein the center feed element is communicatively coupled with a first VAP adjusting arrangement and each of the six edge feed elements is communicatively coupled by way of respective ones of the m:1 power combiners with at least two VAP adjusting arrangements associated with adjacent beams that share the edge element.

7. The spacecraft of claim 6 , wherein the respective ones of the m:1 power combiners are coupled with respective ones of the edge feed elements.

8. The spacecraft of claim 1 , wherein m equals 2 or 3 and n equals 7.

9. The spacecraft of claim 1 , wherein the BFN is configured to provide soft redundancy by allowing reoptimization of the beamforming coefficients in case of a failure of at least one of the power amplifiers.

10. An apparatus comprising:

a payload subsystem for a spacecraft, the payload subsystem including:

a phased array of feed elements configured to illuminate an antenna reflector;

a beam forming network (BFN) coupled with the array of feed elements; and

a plurality of power amplifiers disposed between the BFN and the array of feed elements, wherein:

the phased array of feed elements forms a plurality of beams, each beam being formed by a center feed element, and a plurality of edge feed elements surrounding the center feed element;

the BFN includes a plurality of variable amplitude and phase (VAP) adjusting arrangements disposed between (i) m:1 power combiners that are communicatively coupled with the power amplifiers and (ii) at least one 1:n power splitter;

each VAP adjusting arrangement is communicatively coupled with a single respective one of the feed elements, and at least some of the feed elements are coupled with multiple VAP adjusting arrangements such that the payload subsystem includes more VAP adjusting arrangements than feed elements;

each center feed element is communicatively coupled by way of a single respective VAP adjusting arrangement with a single respective power 1:n power splitter and at least some edge feed elements are communicatively coupled by way of respective ones of the m:1 power combiners with two or more 1:n power splitters; and

m is greater than 1, and n is greater than 2.

11. The apparatus of claim 10 , wherein the spacecraft is configured to receive a ground command and beamforming coefficients of one or more of the VAP adjusting arrangements are correctable by the ground command.

12. The apparatus of claim 11 , wherein a failure of one or more of the power amplifiers is compensatable by correcting, by the ground command, the beamforming coefficients of one or more of the VAP adjusting arrangements.

13. The apparatus of claim 10 , wherein the plurality of power amplifiers are coupled with the array of feed elements.

14. The apparatus of claim 10 , wherein the plurality of feed elements consists of six edge feed elements disposed adjacent to and surrounding the center feed element.

15. The apparatus of claim 14 , wherein the center feed element is communicatively coupled with a first VAP adjusting arrangement and each of the six edge feed elements is communicatively coupled by way of respective ones of the m:1 power combiners with at least two VAP adjusting arrangements associated with adjacent beams that share the edge element.

16. The apparatus of claim 15 , wherein the respective ones of the m:1 power combiners are coupled with respective ones of the edge feed elements.

17. The apparatus of claim 10 , wherein m equals 2 or 3 and n equals 7.

18. The apparatus of claim 10 , wherein the BFN is configured to provide soft redundancy by allowing reoptimization of the beamforming coefficients in case of a failure of at least one of the power amplifiers.