Dual condenser loop heat pipe for satellites with sun-normal radiators
Systems, methods, and apparatus for dual condenser loop heat pipes for satellites with sun-normal radiators are disclosed. In one or more embodiments, a disclosed method for a satellite thermal management system comprises heating, in an evaporator, a liquid to convert the liquid to a vapor. The method further comprises passively circulating within tubing, from the evaporator, the vapor to a first radiator not illuminated by a sun and to a second radiator illuminated by the sun. Also, the method comprises converting the vapor to the liquid when the vapor is within the first radiator not illuminated by the sun. Further, the method comprises passively circulating within the tubing, from the first radiator not illuminated by the sun, the liquid to the evaporator.
1. A method for a satellite thermal management system, the method comprising:
heating, in an evaporator, a liquid to convert the liquid to a vapor;
passively circulating within tubing, from the evaporator, the vapor to a first radiator not illuminated by a sun and to a second radiator illuminated by the sun;
converting the vapor to the liquid when the vapor is within the first radiator not illuminated by the sun; and
passively circulating within the tubing, from the first radiator not illuminated by the sun, the liquid to the evaporator,
wherein the liquid is circulated within the tubing, from the first radiator not illuminated by the sun, to the evaporator via a vapor blocking tee.
2. The method of claim 1 , wherein the first radiator is mounted to an east side of a satellite, and the second radiator is mounted to a west side of the satellite.
3. The method of claim 1 , wherein the first radiator is mounted to a west side of a satellite, and the second radiator is mounted to an east side of the satellite.
4. The method of claim 1 , wherein the vapor is circulated within the tubing, from the evaporator, to the first radiator not illuminated by the sun and to the second radiator illuminated by the sun via a vapor tee.
5. The method of claim 1 , wherein the liquid is a refrigerant.
6. The method of claim 1 , wherein at least one portion of the tubing comprises a flexible segment.
7. The method of claim 6 , wherein the flexible segment is a flex hose.
8. The method of claim 1 , wherein the evaporator is mounted within an interior of a satellite.
9. The method of claim 1 , wherein the liquid is heated by heat conducting from a payload of a satellite.
10. The method of claim 1 , wherein the vapor blocking tee is connected to the first radiator, the second radiator, and the evaporator via the tubing.
11. A satellite thermal management system, the system comprising:
an evaporator configured to heat a liquid to thereby convert the liquid to a vapor;
a first radiator configured such that, when the first radiator is not illuminated by the sun, the vapor within the first radiator is converted to the liquid;
a second radiator; and
tubing connecting the evaporator to the first radiator and to the second radiator,
wherein when the first radiator is not illuminated by the sun and the second radiator is illuminated by the sun, the tubing is configured to passively circulate the vapor from the evaporator to the first radiator and to the second radiator, and to passively circulate the liquid from the first radiator to the evaporator, and
wherein the system is configured to circulate the liquid within the tubing from the first radiator to the evaporator via a vapor blocking tee.
12. The system of claim 11 , wherein the first radiator is mounted to an east side of a satellite, and the second radiator is mounted to a west side of the satellite.
13. The system of claim 11 , wherein the first radiator is mounted to a west side of a satellite, and the second radiator is mounted to an east side of the satellite.
14. The system of claim 11 , wherein the system is configured to circulate the vapor within the tubing from the evaporator to the first radiator and to the second radiator via a vapor tee.
15. The system of claim 11 , wherein the liquid is a refrigerant.
16. The system of claim 11 , wherein at least one portion of the tubing comprises a flexible segment.
17. The system of claim 16 , wherein the flexible segment is a flex hose.
18. The system of claim 11 , wherein the evaporator is mounted within an interior of a satellite.
19. The system of claim 11 , wherein the system is configured to heat the liquid by heat conducting from a payload of a satellite.
20. The system of claim 11 , wherein the vapor blocking tee is connected to the first radiator, the second radiator, and the evaporator via the tubing.