Starshade with attributes facilitating assembly

Patent metadata

Field	Value
Publication number	US-9897723-B2
Application number	US-201615063033-A
Country	US
Kind code	B2
Filing date	Mar 7, 2016
Priority date	Mar 7, 2016
Publication date	Feb 20, 2018
Grant date	Feb 20, 2018

Abstract

An exemplary starshade comprises a tensegrity truss structure having a central hub with radially extending, telescoping booms. Telescoping tension struts connected to the central hub and booms provide a compressive force on the booms during final truss deployment. Opaque petals, not supported by the tensegrity truss structure prior to its final deployment, are each sequentially placed on and attached to the tensegrity truss structure in side by side position to form a concentric ring of petals spaced apart from the central hub. A fan fold covering, not supported by the tensegrity truss structure prior to its final deployment, is placed on and attached to the tensegrity truss structure to form an opaque, concentric inner ring about the central hub. An outer edge of the inner ring is adjacent an interior edge of the concentric ring of petals to block light from the petals to the central hub.

First claim

The invention claimed is:

1. A starshade for deployment and assembly in space and adapted for development and testing in a 1 G environment comprising:
a tensegrity truss structure having:
a central hub;
telescoping booms mounted to the central hub and disposed radially outward to lie in a substantially flat symmetrical conical frustum in a final deployed position; and
telescoping tension struts connected to the central hub and booms to provide a compressive force on the booms towards the central hub when the booms are fully extended in final deployment;

a plurality of opaque petals not supported by the tensegrity truss structure when the booms of the tensegrity truss structure are initially fully extended in deployment, each petal being sequentially deployed and placed on and attached to the tensegrity truss structure in side by side position to form a concentric ring of petals spaced apart from the central hub;
a fan fold covering not supported by the tensegrity truss structure when the booms of the tensegrity truss structure are initially fully extended in deployment, the fan fold covering being placed on and attached to the tensegrity truss structure to form an opaque, concentric inner ring about the central hub, an outer edge of the inner ring being adjacent an interior edge of the concentric ring of petals to block light from the petals to the central hub.

2. The starshade according to claim 1 further comprising:
a first robotic arm, adapted to install and attach the petals and fan fold covering on the tensegrity truss structure, that is not part of a final starshade assembly.

3. The starshade according to claim 1 further comprising:
first and second payloads of first and second rockets, respectively;
the tensegrity truss structure being the first payload and the plurality of opaque petals and the fan fold covering being the second payload, the first and second rockets adapted to launch the respective first and second payload into space.

4. The starshade according to claim 2 further comprising:
first, second, and third payloads of first, second and third rockets, respectively;
the first robotic arm being the first payload, the tensegrity truss structure being the second payload, and the plurality of opaque petals and the fan fold covering being the third payload, the first, second and third rockets adapted to launch the respective first, second and third payloads into space.

5. The starshade according to claim 2 wherein the first robotic arm includes a first tool for holding the petals and fan fold covering as the one robotic arm positions the petals and fan fold covering for attachment on the tensegrity truss structure.

6. The starshade according to claim 5 wherein the first robotic arm includes a second tool for filling seams associated with petals and fan fold covering with opaque material to prevent light leakage via the seams.

7. The starshade according to claim 2 further comprising:
an anchor boom to which the first robotic arm is attached;
a second robotic arm attached to the anchor boom at a location spaced apart from the attachment of the first robotic arm.

8. The starshade according to claim 7 wherein the second robotic arm includes another tool which couples to the tensegrity truss structure and controls the position of the tensegrity truss structure relative to the anchor boom.

9. A method for assembling a starshade comprising the steps of:
deploying a tensegrity truss structure from a stored position to a final operational position, the tensegrity truss structure having booms each with an end mounted to a central hub, the booms being parallel to each other in the stored position;
pivoting the booms radially outward and telescoping each boom in length to lie substantially in a substantially flat symmetrical conical frustum in the final operational position;
exerting a compressive force on the booms towards the central hub when the booms are in the final operational position by tension struts connected to the central hub and booms;
storing a plurality of opaque petals not supported by the tensegrity truss structure while the latter is in its stored position;
sequentially placing and attaching each petal on the tensegrity truss structure in side by side position to form a concentric ring of petals spaced apart from the central hub while the tensegrity truss structure is in its final operational position;
storing a fan fold covering not supported by the tensegrity truss structure while the latter is in its stored position;
placing and attaching the fan fold covering to the tensegrity truss structure to form an opaque, concentric inner ring about the central hub while the tensegrity truss structure is in its final operational position, an outer edge of the inner ring being adjacent and overlapping an interior edge of the concentric ring of petals to block light from the petals to the central hub.

10. The method according to claim 9 further comprising:
using a first robotic arm to install and attach the petals and fan fold covering on the tensegrity truss structure.

11. The method according to claim 9 further comprising:
storing the tensegrity truss structure as a first payload and the plurality of opaque petals and the fan fold covering as a second payload of first and second rockets, respectively, the first and second rockets adapted to launch the respective first and second payloads into space.

12. The method according to claim 10 further comprising:
storing the first robotic arm as a first payload, storing the tensegrity truss structure as the second payload, and storing the plurality of opaque petals and the fan fold covering as a third payload, the first, second, and third payloads carried respectively by first, second and third rockets adapted to launch the first, second and third payloads into space.

13. The method according to claim 10 wherein the first robotic arm includes a first tool that holds the petals and fan fold covering as the one robotic arm positions the petals and fan fold covering for attachment on the tensegrity truss structure.

14. The method according to claim 13 wherein the first robotic arm includes a second tool that installs fasteners to hold the petals to the tensegrity truss structure.

15. The method according to claim 14 wherein the first robotic arms includes a third tool that fills seams associated with petals and fan fold covering with an opaque material to prevent light leakage via the seams.

16. The method according to claim 10 further comprising:
deploying an anchor boom configured to dock with a space station, the first robotic arm being attached to the anchor boom;
using a second robotic arm attached to the anchor boom at a location spaced apart from the attachment of the first robotic arm;
coupling another tool attached to the second robotic arm with the tensegrity truss structure and controlling the position of the tensegrity truss structure relative to the anchor boom by the second robotic arm.

17. The method according to claim 9 wherein all steps are performed in space.

18. The method according to claim 9 wherein all steps are performed in 1G gravity to test the assembly of the starshade.

Assignees

• Northrop Grumman Systems Corp

Inventors

• Dailey Dean R
• Dailey Nicholas B

Classifications

• G02B23/00

  Telescopes, e.g. binoculars; Periscopes; Instruments for viewing the inside of hollow bodies; Viewfinders; Optical aiming or sighting devices · CPC title

• B64G1/105

  Space science · CPC title

• B64G1/54

  Protection against radiation · CPC title

• B64G1/22

  Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles · CPC title

• B64G1/10

  Artificial satellites; Systems of such satellites; Interplanetary vehicles (space shuttles B64G1/14) · CPC title