Systems and methods for cylindrical hall thrusters with independently controllable ionization and acceleration stages
Systems and methods may be provided for cylindrical Hall thrusters with independently controllable ionization and acceleration stages. The systems and methods may include a cylindrical channel having a center axial direction, a gas inlet for directing ionizable gas to an ionization section of the cylindrical channel, an ionization device that ionizes at least a portion of the ionizable gas within the ionization section to generate ionized gas, and an acceleration device distinct from the ionization device. The acceleration device may provide an axial electric field for an acceleration section of the cylindrical channel to accelerate the ionized gas through the acceleration section, where the axial electric field has an axial direction in relation to the center axial direction. The ionization section and the acceleration section of the cylindrical channel may be substantially non-overlapping.
1. A cylindrical Hall thruster, comprising:
a cylindrical channel having a center axial direction and a discharge channel adjacent to a first chassis;
a second chassis coupled to the first chassis via respective chassis flanges, the second chassis comprising a first power source for ionizing at least a portion of ionizable gas in the cylindrical channel to generate ionized gas;
a gas inlet for directing the ionizable gas to an interior of the cylindrical channel, wherein the gas inlet comprises an aperture within at least a portion of the discharge channel; and
a second power source providing an axial electric field for accelerating the portion of ionized gas through the discharge channel of the cylindrical channel, wherein the axial electric field has an axial direction in relation to the center axial direction, and wherein the second power source comprises an anode located within the discharge channel at a location closer to a discharge opening of the cylindrical channel than the first power source and the gas inlet.
2. The cylindrical Hall thruster of claim 1 , wherein the first power source includes one or both of (i) an electron cyclotron resonance (ECR) ionization device, or (ii) an inductive ionization device.
3. The cylindrical Hall thruster of claim 2 , wherein the first power source includes the electron cyclotron resonance (ECR) ionization device, wherein the ECR ionization device includes a radiation source and a transmission line to radiate electromagnetic waves from the radiation source.
4. The cylindrical Hall thruster of claim 3 , wherein the electromagnetic waves comprise microwaves.
5. The cylindrical Hall thruster of claim 3 , wherein the transmission line includes one or more of (i) an antenna, (ii) a microstrip, (iii) a waveguide, or (iv) a coaxial transmission line.
6. The cylindrical Hall thruster of claim 2 , wherein the first power source includes the electron cyclotron resonance (ECR) ionization device, and further comprising:
a dielectric window positioned in the cylindrical channel between the electron cyclotron resonance (ECR) ionization device and the gas inlet, wherein the dielectric window permits electromagnetic waves to pass through to ionize the at least the portion of ionizable gas within the cylindrical channel, wherein the dielectric window prevents the ionizable gas from contacting the first power source.
7. The cylindrical Hall thruster of claim 2 , wherein the first power source comprises a radio frequency (RF) power source applied to inductive coils, the inductive coils formed annularly around at least a portion of the cylindrical channel.
8. The cylindrical Hall thruster of claim 1 , wherein each of the first power source and the second power source are independently controllable.
9. The cylindrical Hall thruster of claim 1 , wherein the second power source further comprises a cathode, the cathode provided externally from the cylindrical channel.
10. The cylindrical Hall thruster of claim 1 , wherein the second power source further comprises a cathode, and wherein the anode and the cathode are coupled to an adjustable DC power source, the adjustable DC power source for controlling a magnitude of the axial electric field.
11. The cylindrical Hall thruster of claim 1 , wherein the ionizable gas is obtained or derived from (i) an external environment or (ii) a container having ionizable gas.
12. The cylindrical Hall thruster of claim 1 , further comprising:
a magnetic device providing a magnetic field having axial and radial components, the magnetic field for enhancing ionization of at least the portion of the ionizable gas within the cylindrical channel, and for supporting the axial electric field for ion acceleration within the cylindrical channel.
13. A method for a cylindrical Hall thruster, comprising:
providing (i) a cylindrical channel having a center axial direction, (ii) a discharge channel adjacent to a first chassis; and (iii) a second chassis coupled to the first chassis via respective chassis flanges, the second chassis comprising a first power source for ionizing at least a portion of ionizable gas in the cylindrical channel to generate ionized gas;
directing, via a gas inlet, the ionizable gas to an interior of the cylindrical channel, wherein the gas inlet comprises an aperture within at least a portion of the discharge channel;
ionizing, by the first power source, the portion of ionizable gas to generate ionized gas; and
accelerating, by a second power source, the portion of ionized gas through the discharge channel of the cylindrical channel, wherein the second power source provides an axial electric field for the acceleration, wherein the axial electric field has an axial direction in relation to the center axial direction, and wherein the second power source comprises an anode located within the discharge channel at a location closer to a discharge opening of the cylindrical channel than the first power source and the gas inlet.
14. The method of claim 13 , wherein the first power source includes one or both of (i) an electron cyclotron resonance (ECR) ionization device, or (ii) an inductive ionization device.
15. The method of claim 14 , wherein the first power source includes the electron cyclotron resonance (ECR) ionization device, wherein the ECR ionization device includes a radiation source and a transmission line to radiate electromagnetic waves from the radiation source.
16. The method of claim 14 , wherein the first power source includes the electron cyclotron resonance (ECR) ionization device, and further comprising:
positioning a dielectric window in the cylindrical channel between the electron cyclotron resonance (ECR) ionization device and the gas inlet, wherein the dielectric window permits electromagnetic waves to pass through to ionize the at least the portion of ionizable gas within the cylindrical channel, wherein the dielectric window prevents the ionizable gas from contacting the first power source.
17. The method of claim 14 , wherein the first power source comprises a radio frequency (RF) power source applied to inductive coils, the inductive coils formed annularly around at least a portion of the cylindrical channel.
18. The method of claim 13 , wherein each of the first power source and the second power source are independently controllable.
19. The method of claim 13 , wherein the second power source further comprises a cathode, the cathode provided externally from the cylindrical channel.
20. The method of claim 13 , further comprising:
providing a magnetic field having axial and radial components, the magnetic field for enhancing ionization of at least the portion of the ionizable gas within the cylindrical channel, and for supporting the axial electric field for ion acceleration within the cylindrical channel.