Modularized feed array arrangement

1. An apparatus comprising:

a modularized feed array arrangement, the feed array arrangement including:

a plurality of radio frequency (RF) radiating elements;

a plurality of waveguides positioned inboard of the plurality of RF radiating elements, each RF radiating element being electrically coupled with an outboard portion of one or more of the waveguides; and

a plurality of modules, each module including a plurality of RF switches, a plurality of amplifiers, and a manifold panel that includes a plurality of RF choke joints; wherein:

an inboard portion of each RF switch is electrically coupled with a respective amplifier; and

each RF choke joint includes a proximal portion electrically coupled with an outboard portion of a respective one of the RF switches and a distal portion electrically coupled with an inboard portion of a respective one of the waveguides.

2. The feed array arrangement of claim 1 , wherein each module is electrically independent from each other module.

3. The feed array arrangement of claim 1 , wherein at least one module is mechanically independent from each other module.

4. The feed array arrangement of claim 1 , wherein at least one module includes one or more heat pipes thermally coupled with at least one of the plurality of amplifiers.

5. The feed array arrangement of claim 1 , wherein the plurality of amplifiers includes one or more of a low noise amplifier (LNA) of a receiver and a solid state power amplifier (SSPA) of a transmitter.

6. The feed array arrangement of claim 1 , wherein at least one module includes a plurality of spare amplifiers.

7. The feed array arrangement of claim 1 , wherein the manifold panel of each module is detachably coupled with a respective subset of the waveguides.

8. The feed array arrangement of claim 1 , wherein:

at least one module includes a transmitter and at least one module includes a receiver; and

at least one RF radiating element is electrically coupled with both the transmitter and the receiver.

9. The feed array arrangement of claim 1 , wherein each of the plurality of RF radiating elements is associated with exactly one respective directed RF beam.

10. The feed array arrangement of claim 1 , wherein each of a plurality of directed RF beams is associated with a respective single one of the plurality of RF radiating elements.

11. The feed array arrangement of claim 1 , wherein:

the feed array arrangement is assembled by fabricating the plurality of modules and mechanically coupling the plurality of fabricated modules with a structural panel by attaching an outboard surface of each manifold panel to an inboard surface of the structural panel; and

attaching the outboard surface of each manifold panel to the inboard surface of the structural panel includes electrically coupling the distal portion of each RF choke joint with the inboard portion of a respective one of a plurality of waveguides.

12. A spacecraft comprising:

an antenna reflector; and

a modularized feed array arrangement, the feed array arrangement including:

a plurality of radio frequency (RF) radiating elements;

a plurality of waveguides positioned inboard of the plurality of RF radiating elements, each RF radiating element being electrically coupled with an outboard portion of one or more of the waveguides; and

a plurality of modules, each module including a plurality of RF switches, a plurality of amplifiers, and a manifold panel that includes a plurality of RF choke joints; wherein:

an inboard portion of each RF switch is electrically coupled with a respective amplifier; and

each RF choke joint includes a proximal portion electrically coupled with an outboard portion of a respective one of the RF switches and a distal portion electrically coupled with an inboard portion of a respective one of the waveguides.

13. The spacecraft of claim 12 , wherein at least one module includes one or more heat pipes thermally coupled with at least one of the plurality of amplifiers.

14. The spacecraft of claim 12 , wherein the manifold panel of each module is detachably coupled with a respective subset of the waveguides.

15. The spacecraft of claim 12 , wherein each of the plurality of RF radiating elements is associated with exactly one respective directed RF beam.

16. The spacecraft of claim 12 , wherein each of a plurality of directed RF beams is associated with a respective single one of the plurality of RF radiating elements.

17. A method comprising

fabricating a plurality of modules, each module including a plurality of RF switches, a plurality of amplifiers, and a manifold panel that includes a plurality of RF choke joints; and

mechanically coupling the plurality of fabricated modules with a structural panel by attaching an outboard surface of each manifold panel to an inboard surface of the structural panel; wherein

an inboard portion of each RF switch is electrically coupled with a respective amplifier,

each RF choke joint includes a proximal portion electrically coupled with an outboard portion of a respective one of the RF switches; and

attaching the outboard surface of each manifold panel to the inboard surface of the structural panel includes electrically coupling a distal portion of each RF choke joint with an inboard portion of a respective one of a plurality of waveguides.

18. The method of claim 17 , wherein an outboard portion of each of the plurality of waveguides is electrically coupled with a respective RF radiating element.

19. The method of claim 18 , wherein each of the plurality of RF radiating elements is associated with exactly one respective directed RF beam.

20. The method of claim 18 , wherein each of a plurality of directed RF beams is associated with a respective single one of the plurality of RF radiating elements.