The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Jul. 16, 2024

Filed:

Oct. 19, 2021
Applicant:

Maxar Space Llc, Palo Alto, CA (US);

Inventors:

Michael Freestone, Woodside, CA (US);

Varouj Baghdasarian, Cupertino, CA (US);

Assignee:

Maxar Space LLC, Palo Alto, CA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
H02S 30/20 (2014.01); B64G 1/44 (2006.01); H02S 10/40 (2014.01); H02S 30/10 (2014.01);
U.S. Cl.
CPC ...
H02S 30/20 (2014.12); B64G 1/443 (2013.01); H02S 10/40 (2014.12); H02S 30/10 (2014.12);
Abstract

A solar array structure for a spacecraft includes one or a pair of flexible blanket or other foldable solar arrays and a deployable frame structure. The deployable frame structure includes a T-shaped yoke structure, a T-shaped end structure, and one or more rigid beams, the T-shaped yoke structure connectable to the spacecraft. When deployed, the frame structure tensions the flexible blanket solar array or arrays between the T-shaped yoke structure and the T-shaped end structure. When stowed, the flexible blanket solar array or arrays are folded in an accordion manner to form a stowed pack or packs between the cross-member arms of the T-shaped yoke structure and the T-shaped end structure, also stowed in its own Z-fold arrangement. The cross-member arms of the T-shaped end structure can include a solar array that can provide power before deployment while the flexible blanket solar array is stowed.


Find Patent Forward Citations

Loading…