Method and apparatus for selectively distributing power in a thruster system

• US 6,031,334 A
• Filed: 08/28/1998
• Issued: 02/29/2000
• Est. Priority Date: 06/17/1998
• Status: Expired due to Term

• Current Assignee: Aerojet Rocketdyne Inc. (L3Harris Technologies, Inc.)
• Original Assignee: Primex Technologies Inc (General Dynamics Corporation)
• Inventors: Meyer, Steven D.
• Primary Examiner(s): Le, Hoanganh
• Assistant Examiner(s): Lee, Wilson
• Application Number:
  US09/143,294
• Time in Patent Office: 550 Days
• Field of Search: 315/111.81, 315/111.21, 315/111.91, 315/106, 315/111.01, 315/344, 313/359.1, 60/202
• US Class Current: 315/111.01
• CPC Class Codes: F03H 1/0018 Arrangements or adaptations of power supply systems for cosmonautic vehicles B64G1/42

Abstract

A single power control circuit selectively distributes power from a power supply to cathode heater, cathode keeper and thruster magnets of a thruster. The power control circuit utilizes a plurality of switching devices to direct power to one or more of the heater, keeper, and magnet components.

Claims

1. A control system comprising:

a thruster assembly for producing a discharge;

a cathode assembly for producing an electron beam, the cathode assembly having emitter, heater and keeper elements;

at least one magnetic device operatively associated with the thruster assembly for generating a magnetic field to control the discharge;

a power supply for supplying power to the system; and

a power distribution circuit coupled to the cathode assembly, the at least one magnetic device, and the power supply, for selectively providing power to the keeper, the heater and the at least one magnetic device.

2. The control system as claimed in claim 1 wherein the power distribution circuit further comprises:

a power control circuit for receiving power from the power supply; and

at least one switching device for providing current paths from the power control circuit to the heater or the keeper or the at least one magnetic device or combination thereof.

3. The control system as claimed in claim 2 wherein the power distribution circuit further comprises:

a sequencing logic unit coupled to the power control circuit and the at least one switching device for providing control signals to the power control circuit and the at least one switching device.

4. The control system as claimed in claim 2 further comprising:

an anode coupled to the cathode assembly for providing a voltage having a polarity opposite a polarity of the emitter; and

an anode power supply coupled to the power distribution circuit for supplying power to the anode.

5. The control system as claimed in claim 2 wherein a first one of the at least one switching device provides an electrical current path from the power control circuit to the at least one magnetic device when the first switching device is in a non-conducting state.

6. The control system as claimed in claim 5 wherein a second one of the at least one switching device provides a current path from the power control circuit to the heater when the path from the power control circuit to the heater when the second switching device is in a conducting state.

7. The control system as claimed in claim 6 wherein a third one of the at least one switching device provides a current path from a positive terminal of the power control circuit to a negative terminal of the power control circuit when the third switching device is in a conducting state thereby preventing power from reaching the keeper.

8. A control apparatus comprising:

a power supply for providing a source of power;

a power distribution circuit coupled to the power supply; and

a cathode assembly coupled to the power distribution circuit for discharging an electron beam, the cathode assembly enclosing heater, emitter and keeper elements;

wherein the power distribution circuit receives power from the power supply and selectively distributes the received power to one or both of the heater and the keeper elements.

9. The control apparatus as claimed in claim 8 further comprising:

at least one magnetic device operably associated with the cathode assembly for generating a magnetic field to control an ion beam discharged from a thruster assembly.

10. The control apparatus of claim 9 wherein the at least one magnetic device is coupled to the power distribution circuit;

and

the power distribution circuit selectively providing power received from the power supply to the at least one magnetic device.

11. The control apparatus as claimed in claim 9 wherein the at least one magnetic device receives power from a discharge path.

12. The control apparatus as claimed in claim 8 wherein the power distribution circuit further comprises:

a power control circuit for supplying a controlled amount of power to the cathode assembly; and

at least one switching device coupled to the power control circuit for selectively providing current paths from the power control circuit to the cathode assembly in response to control signals transmitted from the power control circuit.

13. The control apparatus as claimed in claim 12 wherein a first one of the at least one switching device provides an electrical current path from the power control circuit to the heater when the first switching device is in a conducting state;

and

a second one of the at least one switching device provides an electrical current path from a positive terminal of the power control circuit to a negative terminal of the power control circuit when the second switching device is in a conducting state thereby preventing power from reaching the keeper.

14. The control apparatus as claimed in claim 12 wherein the power distribution circuit further comprises:

a sequencing logic unit coupled to the power control circuit and the at least one switching device, for providing command signals to the power control circuit and control signals to the at least one switching device.

15. The control apparatus as claimed in claim 12 wherein the power control circuit generates an ignition voltage and transmits the ignition voltage to the keeper.

16. The control apparatus as claimed in claim 12 further comprising:

a thruster control circuit coupled to the power distribution circuit for providing input signals to the power distribution circuit;

a discharge power supply coupled to the cathode assembly and the thruster control circuit for providing anode current;

a thruster coupled to the discharge power supply and the power distribution circuit for producing thrust.

17. The control apparatus as claimed in claim 8 further comprising:

a diode for providing current to the cathode assembly when conducting.

18. The control apparatus as claimed in claim 8 further comprising:

one or more auxiliary power supplies coupled to the power distribution circuit for providing additional electrical power to the power distribution circuit.

19. A method for controlling discharge components comprising:

providing an electron beam generating device;

providing a magnetic field generating device;

providing a power source; and

distributing power from said power source to the electron beam generating device and/or the magnetic field generating device by operation of a plurality of switching devices.

20. The method as claimed in claim 19 further comprising:

coupling an anode to the electron beam generating device.

21. The method as claimed in claim 19 further comprising:

providing at least one auxiliary power source.