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:
Aug. 29, 2017

Filed:

Apr. 01, 2015
Applicant:

Worldvu Satellites Limited, St Helier, Jersey, GB;

Inventors:

Alexander D. Smith, San Jose, CA (US);

Armen Askijian, Sunnyvale, CA (US);

Daniel W. Field, Sunnyvale, CA (US);

James Grossman, Sunnyvale, CA (US);

Assignee:

WORLDVU SATELLITES LIMITED, St Helier, Jersey, GB;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64G 1/52 (2006.01); B64G 1/58 (2006.01); B64G 1/10 (2006.01); B64G 1/50 (2006.01); B64G 1/24 (2006.01); B64G 1/66 (2006.01); B64G 1/42 (2006.01);
U.S. Cl.
CPC ...
B64G 1/58 (2013.01); B64G 1/1007 (2013.01); B64G 1/242 (2013.01); B64G 1/50 (2013.01); B64G 1/503 (2013.01); B64G 1/66 (2013.01); B64G 1/425 (2013.01);
Abstract

A method for thermally stabilizing a communication satellite in orbit around the Earth relies on the discrete rotational symmetry of the pattern of antenna beams of the satellite. Exploiting the symmetry, the orientation of the satellite is changed from time to time by rotating the satellite through a symmetry angle of the rotational symmetry. Because of the symmetry, the beam pattern is unchanged after the rotation; but, because the rotation angle is less than 360°, a different side of the satellite is exposed to sunlight. The use of different thermal radiators and thermal shields on different sides of the satellite means that the thermal budget of the satellite is different after the rotation. By judiciously applying rotations as needed, as the orbit's orientation relative to the Sun evolves in time, it is possible to achieve effective control on the thermal budget of the satellite.


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