Satellite with a thermal switch and associated methods

Patent metadata

Field	Value
Publication number	US-10865000-B2
Application number	US-201715687808-A
Country	US
Kind code	B2
Filing date	Aug 28, 2017
Priority date	Aug 28, 2017
Publication date	Dec 15, 2020
Grant date	Dec 15, 2020

Abstract

A satellite includes a satellite housing, a temperature sensitive component carried by the satellite housing, and a thermal radiator carried by the satellite housing. A thermal switch is movable between a coupled state and a decoupled state. In the coupled state, the temperature sensitive component and the thermal radiator are thermally coupled. In the decoupled state, the temperature sensitive component and the thermal radiator are thermally decoupled.

First claim

That which is claimed is:

1. A satellite comprising:
a satellite housing;
a temperature sensitive component carried by said satellite housing;
a thermal radiator carried by said satellite housing;
an electrically powered heater configured to heat said temperature sensitive component;
a thermal switch movable between a coupled state with said temperature sensitive component and said thermal radiator being thermally coupled, and a decoupled state with said temperature sensitive component and said thermal radiator being thermally decoupled;
a temperature sensor configured to sense a temperature of said temperature sensitive component; and
a controller configured to
move said thermal switch to the coupled state when the sensed temperature of said temperature sensitive component is above a temperature range, and
operate said electrically powered heater to heat said temperature sensitive component and move the thermal switch to the decoupled state when the sensed temperature of said temperature sensitive component is below the temperature range.

2. The satellite according to claim 1 wherein said thermal switch, when in the decoupled state, defines a vacuum gap between said temperature sensitive component and said thermal radiator.

3. The satellite according to claim 1 wherein said thermal switch comprises an electromagnetically operated actuator.

4. The satellite according to claim 3 wherein said electromagnetically operated actuator comprises a solenoid coil, and at least one flexure mount coupled between said temperature sensitive component and said thermal radiator.

5. The satellite according to claim 3 wherein said electromagnetically operated actuator comprises at least one solenoid fastener coupled between said temperature sensitive component and said thermal radiator.

6. The satellite according to claim 1 further comprising a compressible thermal interface layer between said temperature sensitive component and said thermal radiator when said thermal switch is in the coupled state.

7. The satellite according to claim 1 wherein said temperature sensitive component comprises an electronic circuit device.

8. The satellite according to claim 1 wherein said temperature sensitive component comprises a battery.

9. A satellite comprising:
a satellite housing;
a temperature sensitive component carried by said satellite housing;
a thermal radiator carried by said satellite housing;
an electrically powered heater configured to heat said temperature sensitive component;
a thermal switch movable between a coupled state with said temperature sensitive component and said thermal radiator being thermally coupled, and a decoupled state with said temperature sensitive component and said thermal radiator having a vacuum gap therebetween, said thermal switch comprising an electromagnetically operated actuator;
a temperature sensor configured to heat said temperature sensitive component; and
a controller configured to
move said thermal switch to the coupled state when the sensed temperature of said temperature sensitive component is above a temperature range, and
operate said electrically powered heater to heat the temperature sensitive component and move the thermal switch to the decoupled state when the sensed temperature of said temperature sensitive component is below the temperature range.

10. The satellite according to claim 9 wherein said electromagnetically operated actuator comprises a solenoid coil, and at least one flexure mount coupled between said temperature sensitive component and said thermal radiator.

11. The satellite according to claim 9 wherein said electromagnetically operated actuator comprises at least one solenoid fastener coupled between said temperature sensitive component and said thermal radiator.

12. The satellite according to claim 9 further comprising a compressible thermal interface layer between said temperature sensitive component and said thermal radiator when said thermal switch is in the coupled state.

13. The satellite according to claim 9 wherein said temperature sensitive component comprises at least of an electronic circuit device and a battery.

Assignees

• Harris Corp

Inventors

• Newlin Christopher R
• Mast Alan W

Classifications

• H01H37/02

  Details · CPC title

• B64G1/503 Primary

  Radiator panels · CPC title

• B64G1/10

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

• B64G1/66

  Arrangements or adaptations of apparatus or instruments, not otherwise provided for · CPC title

• B64G1/50 Primary

  for temperature control · CPC title