Foldable radio wave antenna deployment apparatus for a satellite

1. An antenna, comprising:

a parabola-shaped, flexible reflector member having a peripheral rim;

one or more radial ribs embedded in the flexible reflector member and arranged to bias the reflector member in an open state; and

a generally circular tension member defining a central opening, the generally circular tension member having a having a circumferential edge that is coupleable with the peripheral rim of the flexible reflector member such that generally circular tension member spans an interior space defined by the peripheral rim, the generally circular tension member being configured to draw the peripheral rim of the flexible reflector member centrally such that an edge of the peripheral rim maintains a generally circular shape.

2. The antenna of claim 1 , wherein the radial ribs are embedded in laminate forming the flexible reflector member.

3. The antenna of claim 1 , wherein the radial ribs are embedded between a fiber composite layer and a elastomer layer of the reflector.

4. The antenna of claim 1 , wherein the one or more radial ribs are composed of wire.

5. The antenna of claim 4 , wherein the wire is 32-gauge.

6. The antenna of claim 1 , wherein the one or more ribs are composed of a material with low conductivity.

7. The antenna of claim 6 , wherein the material is fiberglass/phenolic composite.

8. An antenna system, comprising:

a parabola-shaped, flexible reflector member;

one or more radial ribs embedded in the flexible reflector member and arranged to be foldable to a closed state; and

a retaining assembly comprising:

a mounting plate;

a plurality of retaining leaves positioned around an exterior of the flexible reflector member, wherein a proximal end of each of the plurality of retaining leaves is pivotally coupled with the mounting plate and a distal end of each of the retaining leaves is unconstrained; and

a collar member that is coupled with the mounting plate such that a distance between the mounting plate and the collar member is adjustable, the collar member defining an opening having an edge that is configured to contact an outer surface of each of the plurality of retaining leaves, wherein:

the retaining assembly is configured to move between:

an deployed configuration in which the mounting plate and the collar member are positioned proximate to one another to lower a contact position of the collar member with the outer surfaces of the plurality of retaining leaves such that the plurality of retaining leaves pivot toward the mounting plate, thereby allowing the flexible reflector member to expand to an opened state; and

a retained configuration in which the mounting plate and the collar member are positioned apart from one another to raise a contact position of the collar member with the outer surfaces of the plurality of retaining leaves such that the plurality of retaining leaves pivot toward the flexible reflector member, thereby causing the flexible reflector member to fold.

9. The antenna system of claim 1 , further comprising a retaining assembly adapted for retaining the flexible reflector member in the closed state.

10. The antenna system of claim 9 , wherein the retaining assembly comprises a plurality of retaining leaves pivotally mounted perpendicular to a mounting plate.

11. The antenna system of claim 10 , wherein the retaining leaves are biased to rotate outward from the flexible reflector member.

12. The antenna system of claim 10 , wherein the mounting plate comprises an opening through which signal feed may be conveyed to a feed horn.

13. The antenna system of claim 12 , wherein the mounting plate is moveably coupled to a satellite.

14. The antenna system of claim 13 , wherein upon receiving a signal from a satellite control system of the satellite, the reflector member deploys from its closed state.

15. The antenna system of claim 8 , further comprising a motor coupled with the retaining system, wherein the motor controls the relative positions of the mounting plate and the collar member.

16. The antenna system of claim 15 , wherein the retaining system is coupled with a satellite, and wherein the motor is configured to move the retaining system from the retained configuration to the deployed configuration upon receiving a signal from a satellite control system of the satellite.