IP Library › Granted Patent US 12,548,915
Granted Patent B2
US 12,548,915 · App. 18/606,423 · Granted Feb 10, 2026

Deployable antenna reflector

Inventors: Juan M. Fernandez (Norfolk, VA); Andrew F. Paddock (Newport News, VA); Kevin DeMarco (Yorktown, VA)
Assignee: United States of America as represented by the Administrator of NASA
H01Q15/20H01Q1/288H01Q15/148H01Q15/16
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Quick Facts
Patent No.
US 12,548,915
App. No.
18/606,423
Granted
Feb 10, 2026
Kind
B2
Abstract

Self-deploying reflector array architectures include stacked multiple panels attached to a central panel by sets of heat actuated flexible hinges on their non-functional sides create surface of revolution, cylindrical and flat reflector arrays in accordance with panel curvature. Robotic in-space assembly of multiple smaller arrays allows for creation of reflector array of 10 or more meters to support S-band and above RF (≥2 GHz) transmission.

Claims (23)

1 . An antenna reflector array having at least a stowed position and a deployed position, the array comprising:

multiple panels and a central panel, each of the multiple and central panels including a functional side and a non-functional side, wherein in the stowed position, the multiple and central panels are in a compact configuration;

at least one heat actuated flexible hinge formed of a shape memory composite (“SMC”) substrate, each of the at least one flexible hinge being connected at a first end thereof to a non-functional side of one of the multiple panels and at a second end thereof to the non-functional side of the central panel, the at least one heat actuated flexible hinge being controllable between a first shape and a second shape; and

further wherein, when each of the at least one heat actuated flexible hinge changes from the first shape to the second shape, the multiple panels connected thereto are moved from a first position to a second position.

2 . The antenna reflector array of claim 1 , wherein each of the at least one flexible hinge includes a controllable heater for providing heat to a heat actuated flexible hinge to actuate the heat actuated flexible hinge between the first and second shapes.

3 . The antenna reflector array of claim 1 , wherein each of the heat actuated flexible hinges is tubular.

4 . The antenna reflector array of claim 1 , wherein each of the multiple panels and the central panel are a rigid construction.

5 . The antenna reflector array of claim 1 , wherein at least one of the heat actuated flexible hinges includes a hinge having a single hinge point and remaining the of heat actuated flexible hinges include hinges having dual hinge points.

6 . The antenna reflector array of claim 1 , wherein the compact configuration is a stacked configuration, wherein the functional side of the central panel faces away from the non-functional sides of the multiple panels.

7 . The antenna reflector array of claim 6 , wherein the functional side of each of the multiple and central panels is curved; and

wherein when in the stacked configuration the curved functional side of the central panel faces an opposite direction from the curved functional sides of the multiple panels and when in the deployed position the curved functional side of the central panel faces a same direction as the curved functional sides of the multiple panels.

8 . The antenna reflector array of claim 7 , wherein the curved functional side of each of the multiple and central panels is a single curve; and

further wherein when in the deployed position, the antenna reflector array is cylindrical.

9 . The antenna reflector array of claim 7 , wherein the curved functional side of each of the multiple and central panels is a double curve; and

further wherein when in the deployed position the antenna reflector array is a surface of revolution such as a paraboloid.

10 . The antenna reflector array of claim 6 , wherein the functional side of each of the multiple and central panels is flat; and

further wherein when in the deployed position the antenna reflector array is flat.

11 . The antenna reflector array of claim 6 , wherein when in the stacked configuration, all of the multiple panels are stacked below the central panel and deployment of the multiple panels occurs from the outermost panel in the stack to the innermost panel in the stack with respect to the central panel.

12 . The antenna reflector array of claim 6 , wherein when in the stacked configuration, at least one of the multiple panels is stacked above the central panel and remaining multiple panels are stacked below the central panel.

13 . The antenna reflector array of claim 6 , wherein when in the stacked configuration, each of the multiple panels is concentrically aligned with the central panel.

14 . The antenna reflector array of claim 6 , wherein when in the stacked configuration, the stack is staggered and a first edge of each of the multiple panels is offset a distance D o from a first edge of the central panel and an offset distance D o is different for each of the multiple panels.

15 . The antenna reflector array of claim 14 , wherein the offset distance D o for each of the multiple panels is equal to a vertical distance D v between each of the multiple panels and the central panel in the stack.

16 . The antenna reflector array of claim 1 , wherein when in the compact configuration, each of the multiple panels is held at an approximately 90 degree angle to the central panel by the at least one of the heat actuated flexible hinges.

Assignments (3)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 23, 2025
From: FERNANDEZ, JUAN MIGUEL; PADDOCK, ANDREW F.
To: UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF NASA
Reel/Frame 069979/0638 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 23, 2025
From: DEMARCO, KEVIN
To: ANALYTICAL MECHANICS ASSOCIATES
Reel/Frame 069979/0746 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 23, 2025
From: ANALYTICAL MECHANICS ASSOCIATES
To: UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF NASA
Reel/Frame 069979/0831 →
Continuity (3)
Provisional Application 63452712 · Mar 17, 2023
Provisional Application 63452713 · Mar 17, 2023
Related Publication 20240313418A1 · Sep 19, 2024
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