Patent ID: 11962272
Assignee: MAXAR SPACE LLC
Field: Transport (Mechanical engineering)
Classification: CPC H  B | IPC B  H

Claim 13:
14. The spacecraft of claim 11, wherein the deployable frame structure comprises:
a T-shaped yoke structure having a central member and a cross-member arm, the cross-member arm attached to the foldable solar array at a first end in the first direction and the central member configured to mount to a spacecraft;
a T-shaped end structure having a central member and a cross-member arm, the cross-member arm attached to the foldable solar array at a second end in the first direction;
one or more rigid beams; and
a plurality of frame hinges connecting the T-shaped yoke structure, the one or more rigid beams, and the T-shaped end structure, including a first frame hinge connected to the T-shaped yoke structure and a second frame hinge connected to an end of the central member of the T-shaped end structure.