Artificial satellite

Patent metadata

Field	Value
Publication number	US-10155597-B2
Application number	US-201615750980-A
Country	US
Kind code	B2
Filing date	Aug 10, 2016
Priority date	Aug 10, 2015
Publication date	Dec 18, 2018
Grant date	Dec 18, 2018

Abstract

Disclosed is an artificial satellite including one face from the North face and the South face supporting at least one main radiator having an outer face turned towards space and an inner face opposite the outer face. The satellite includes a bearing structure carrying the North face, the South face, the East face and the West face. At least one part of the at least one main radiator protrudes from at least one face from the East face and the West face. The inner face of the at least one protruding part is covered with a high infrared emissivity material. The value of the dimension of the at least one protruding part is between 19% and 50% of the value of the distance between the East and West faces.

First claim

The invention claimed is:

1. An artificial satellite comprising:
a North face;
a South face opposite the North face;
an East face;
a West face opposite the East face; and
a bearing structure carrying the North face, the South face, the East face and the West face,
wherein said satellite has a longitudinal direction which extends in a launch direction, a first direction perpendicular to the longitudinal direction and a second direction perpendicular to the longitudinal direction and the first direction, said North and South faces being perpendicular to said first direction, said East and West faces being perpendicular to said second direction, the distance between the East and West faces measured along the second direction being less than the distance between the North and South faces measured along the first direction, one face from the North face and the South face, supporting at least one main radiator that has an outer face turned towards space and an inner face opposite the outer face, at least one part of said at least one main radiator protruding in relation to at least one of the East face and the West face, and
the inner face of said at least one protruding part is covered with a material having an infrared emissivity higher than 0.7, a value of a dimension of said at least one protruding part measured along the second direction being between 19% and 50% of the value of the distance between the East and West faces measured along the second direction.

2. The artificial satellite according to claim 1 , wherein the value of the dimension of said at least one protruding part measured along the second direction is between 23% and 33% of the value of the distance between the East and West faces measured along the second direction.

3. The artificial satellite according to claim 1 , wherein a part of the at least one main radiator protrudes in relation to the East face and another part of the at least one main radiator protrudes in relation to the West face.

4. The artificial satellite according to claim 1 , wherein the inner face of the at least one protruding part of said main radiator is coated with a reflective material.

5. The artificial satellite according to claim 4 , wherein the reflective material is an optical solar reflector type material.

6. The artificial satellite according to claim 1 , wherein the inner face of at least one protruding part of said main radiator is coated with white paint.

7. The artificial satellite according to claim 1 , wherein the inner face of at least one protruding part of said main radiator is coated with black paint.

8. The artificial satellite according to claim 1 , wherein the dimension between an end of the North face and an end of the South face diametrically opposite is less than 3.9 meters.

9. The artificial satellite according to claim 1 , wherein the bearing structure is a cylindrical structure that has a diameter substantially equal to 1.666 meters, and
wherein the distance between the East and West faces measured along the second direction is more than 1.7 meters.

10. The artificial satellite according to claim 1 , further comprising at least one antenna reflector,
wherein said at least protruding part has a lateral notch crossed by a part of said at least one antenna reflector.

11. The artificial satellite according to claim 1 , further comprising solar panels attached to the North face and to the South face, a dimension of the solar panels along the second direction being substantially equal to the dimension of the North face and to the dimension of the South face, along said second direction.

Assignees

• Airbus Defence & Space Sas

Inventors

• Cael Philippe
• Walker Andrew
• Mena Fabrice

Classifications

• B64G1/10

  Artificial satellites; Systems of such satellites; Interplanetary vehicles (space shuttles B64G1/14) · CPC title

• B64G1/226

  Special coatings for spacecraft · CPC title

• B64G1/1007 Primary

  Communications satellites · CPC title

• B64G1/503

  Radiator panels · CPC title

• B64G1/44

  using radiation, e.g. deployable solar arrays · CPC title