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:
Feb. 22, 2022

Filed:

Jun. 21, 2019
Applicants:

Airbus Defence and Space Sas, Toulouse, FR;

Airbus Defence and Space Netherlands B.v, Leiden, NL;

Inventors:

Fabrice Mena, Toulouse, FR;

Bruin Benthem, Toulouse, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64G 1/58 (2006.01); B64G 1/22 (2006.01); B64G 1/10 (2006.01); B64G 1/44 (2006.01); B64G 1/50 (2006.01);
U.S. Cl.
CPC ...
B64G 1/58 (2013.01); B64G 1/10 (2013.01); B64G 1/222 (2013.01); B64G 1/44 (2013.01); B64G 1/503 (2013.01);
Abstract

A radiative fin for a spacecraft is disclosed having an end fitting of heat conductive material, configured to be mounted on the spacecraft, a flexible radiative laminate, connected to the end fitting at one end and having an opposite free end, at least one pyrolytic graphite sheet, and at least one heat emission layer in contact with the pyrolythic graphite sheet on at least part of the surface of the pyrolythic graphite sheet, and a flexible rod, extending from the end fitting along at least part of a side of the flexible radiative laminate and being affixed to the latter. The flexible rod is adapted to occupy a folded position and a deployed position and to exert, while in the folded position, a deployment torque adapted to bring the flexible rod back to the deployed position.


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