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:
Dec. 06, 2022

Filed:

Mar. 07, 2019
Applicant:

Oxford Space Systems Limited, Harwell, GB;

Inventors:

Michael David Lawton, Harwell, GB;

Zhong You, Old Marston, GB;

Deborah Fellows, Harwell, GB;

Assignee:

Oxford Space Systems Limited, Oxfordshire, GB;

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64G 1/22 (2006.01); B64G 1/24 (2006.01); B64G 1/42 (2006.01); B64G 1/64 (2006.01); B64G 1/66 (2006.01);
U.S. Cl.
CPC ...
B64G 1/222 (2013.01); B64G 1/244 (2019.05); B64G 1/428 (2013.01); B64G 1/641 (2013.01); B64G 1/66 (2013.01); B64G 2001/643 (2013.01);
Abstract

A spacecraft is disclosed, comprising a deployable spacecraft body () comprising a plurality of sub-systems (-) for controlling operations of the spacecraft, and a plurality of panels () and a plurality of hinges (-) each connecting adjacent ones of the plurality of panels, the hinges being arranged to permit the plurality of panels to be folded into a stowed configuration and unfolded into a deployed configuration, wherein the plurality of sub-systems are fixed to and supported by one or more of the plurality of panels. By forming the body of the spacecraft from a deployable structure, the overall size of the spacecraft can be significantly reduced in the stowed configuration. In some embodiments, a plurality of the spacecraft in the stowed configuration can be combined into a modular spacecraft assembly prior to launch, with data and power connections between the plurality of stowed spacecraft being used to transfer power from, and data to, a payload monitoring unit on the launch vehicle.


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