Thermally managed electric propulsion systems

1. An electric propulsion (EP) system, comprising:

a discharge chamber with a longitudinal extension according to an axial direction of the EP system; and

a magnetic circuit for generation in the discharge chamber of a magnetic field according to a radial direction of the EP system,

wherein the magnetic circuit comprises:

a monolithic structure with an integrated continuous serpentine channel for provision of an embedded oscillating heat pipe (OHP).

2. The electric propulsion (EP) system of claim 1 , wherein:

the monolithic structure includes at least one of: a backplate; an outer core; or an inner core of the magnetic circuit.

3. The electric propulsion (EP) system of claim 1 , wherein:

the monolithic structure includes a backplate and an inner core of the magnetic circuit that are monolithically integrated into one structure.

4. The electric propulsion (EP) system of claim 1 , wherein:

the monolithic structure includes a backplate and an outer core of the magnetic circuit that are monolithically integrated into one structure.

5. The electric propulsion (EP) system of claim 1 , wherein:

the monolithic structure includes a backplate, an inner core, and an outer core of the magnetic circuit that are monolithically integrated into one structure.

6. The electric propulsion (EP) system of claim 1 , wherein:

the monolithic structure is made from a single magnetic material having a coercivity of less than 1000 A/m.

7. The electric propulsion (EP) system of claim 1 , wherein:

the monolithic structure is made from at least one single magnetic material having a coercivity of less than 1000 A/m.

8. The electric propulsion (EP) system of claim 1 , wherein:

the continuous serpentine channel is formed inside of the monolithic structure and at an offset from a center axis of the EP system.

9. The electric propulsion (EP) system of claim 8 , wherein:

the continuous serpentine channel is a sealed channel that is filled with a working fluid.

10. The electric propulsion (EP) system of claim 8 , wherein:

the continuous serpentine channel forms a path of the embedded OHP that alternates between hot and cold regions of the EP system.

11. The electric propulsion (EP) system of claim 8 , wherein:

the continuous serpentine channel includes a plurality of major channel segments, each major channel segment of the plurality of major channel segments extending along the axial direction or the radial direction of the EP system.

12. The electric propulsion (EP) system of claim 11 , wherein:

the continuous serpentine channel further includes a plurality of minor channel segments, each minor channel segment of the plurality of minor channel segments joining two major channel segments of the plurality of major channel segments.

13. The electric propulsion (EP) system of claim 12 , wherein:

the plurality of minor channel segments follows an outer circular contour of an inner or outer core of the magnetic circuit.

14. The electric propulsion (EP) system of claim 12 , wherein:

the plurality of minor channel segments follows an outer or inner circular contour of a backplate of the magnetic circuit.

15. The electric propulsion (EP) system of claim 1 , wherein:

the discharge chamber is annular about a center axis of the EP system, the center axis being the center axis according to the axial direction of the EP system, and

the monolithic structure radially and axially surrounds the discharge chamber.

16. The electric propulsion (EP) system of claim 15 , wherein:

the embedded OHP includes alternating axial paths arranged radially inwardly and radially outwardly of the discharge chamber.

17. The electric propulsion (EP) system of claim 1 , wherein:

the embedded OHP includes a sealed working fluid, the sealed working fluid comprising one or more of: Glycerin, Heptane, Dowtherm G (a mixture of di- and tri-aryl compounds), Mercury, Sulphur, Cesium, NaK, Sodium, Potassium or Water.

18. The electric propulsion (EP) system of claim 1 , wherein:

the EP system is a Hall effect thruster.

19. The electric propulsion (EP) system of claim 1 , further comprising:

a secondary thermal management system that is thermally coupled to the monolithic structure, the secondary thermal management system configured to:

extract heat from the monolithic structure of the EP system,

conduct extracted heat to a remote radiator, and

reject heat through the remote radiator.

20. The electric propulsion (EP) system of claim 19 , wherein:

the secondary thermal management system includes a cylindrical heat exchanger that is thermally coupled to an outer core of the magnetic circuit that is part of the monolithic structure.

21. The electric propulsion (EP) system of claim 19 , wherein:

the secondary thermal management system includes a baseplate heat exchanger that is thermally coupled to a backplate of the magnetic circuit that is part of the monolithic structure.

22. A method for thermal management of an electric propulsion (EP) system, the method comprising:

fabricating a magnetic circuit of the EP system as a monolithic structure;

based on the fabricating, forming a continuous serpentine channel inside of the monolithic structure, thereby obtaining an integrated continuous serpentine channel;

filling the integrated continuous serpentine channel with a working fluid;

sealing the integrated continuous serpentine channel, thereby embedding an oscillating heat pipe (OHP) in the magnetic circuit;

forming a discharge chamber of the EP system within an annular region provided by the monolithic structure of the magnetic circuit, the magnetic circuit configured to generate a radial magnetic field inside of the discharge chamber; and

based on the embedding of the OHP, thermally managing the EP system by increasing a thermal conductivity of the magnetic circuit.

23. The method according to claim 22 , wherein:

the fabricating of the magnetic circuit includes fabricating based on additive manufacturing.