Micro-cathode thruster and a method of increasing thrust output for a micro-cathode thruster

Patent metadata

Field	Value
Publication number	US-9517847-B2
Application number	US-201414503814-A
Country	US
Kind code	B2
Filing date	Oct 1, 2014
Priority date	Apr 6, 2010
Publication date	Dec 13, 2016
Grant date	Dec 13, 2016

Abstract

A magnetically enhanced micro-cathode thruster assembly provides long-lasting thrust. The micro-cathode thruster assembly includes a tubular housing, a tubular cathode, an insulator, an anode and a magnetic field. The tubular housing includes an open distal end. The tubular cathode is housed within the housing and includes a distal end positioned proximate the open distal end of the housing. The insulator is in contact with the cathode forming an external cathode-insulator interface. The anode is housed within the housing, proximate the open distal end of the housing. The magnetic field is positioned at or about the external cathode-insulator interface and has magnetic field lines with an incidence angle of about 20 to about 30 degrees and preferably about 30 degrees relative to the external cathode-insulator interface.

First claim

We claim:

1. A micro-cathode thruster assembly comprising:
a tubular housing having an open distal end;
a tubular cathode housed within the housing, the cathode having a distal end positioned proximate the open distal end of the housing;
an insulator in contact with the cathode forming an external cathode-insulator interface;
an anode housed within the housing and proximate the open distal end of the housing; and
a magnetic field having magnetic field lines positioned at the external cathode-insulator interface at an incidence angle of about 20 degrees to about 30 degrees relative to the external cathode-insulator interface.

2. The micro-cathode thruster assembly of claim 1 , wherein the anode is a tubular anode or a cylindrical anode.

3. The micro-cathode thruster assembly of claim 2 , wherein the insulator is in contact with a distally facing end of the cathode, and between the cathode and the anode.

4. The micro-cathode thruster assembly of claim 3 , wherein the anode is positioned distal to the cathode and the insulator.

5. The micro-cathode thruster assembly of claim 1 , wherein the magnetic field has a magnetic field strength of about 0.1 tesla to about 0.3 tesla.

6. The micro-cathode thruster assembly of claim 1 , further comprising a biasing member biasing the cathode in a distal direction.

7. The micro-cathode thruster assembly of claim 6 , wherein the biasing member is a spring that includes:
a distal end engaged with a proximal end of the cathode; and
a proximal end engaged with a base of the housing.

8. The micro-cathode thruster assembly of claim 1 , wherein the cathode has a longitudinal axis and the magnetic field lines are oriented at an incidence angle of about 20 degrees to about 30 degrees relative to the longitudinal axis of the cathode at the external cathode-insulator interface.

9. The micro-cathode thruster assembly of claim 1 , wherein the magnetic field lines are oriented at an incidence angle of about 30 degrees relative to the external cathode-insulator interface.

10. The micro-cathode thruster assembly of claim 1 , wherein the housing includes an abutment proximate the open distal end for arresting movement of the cathode in a distal direction.

11. The micro-cathode thruster assembly of claim 1 , wherein the insulator comprises a conductive film forming the external cathode-insulator interface.

12. The micro-cathode thruster assembly of claim 11 , wherein the conductive film is a metal or carbon.

13. A micro-cathode thruster comprising:
a power unit that includes:
a voltage source,
an inductor connected to the voltage source, and
a switch connected to the voltage source and the inductor; and

a thruster assembly connected to the power unit, the thruster assembly including:
a tubular housing having an open distal end,
a tubular cathode housed within the housing, the cathode having a distal end positioned proximate the open distal end of the housing,
an insulator in contact with the cathode forming an external cathode-insulator interface,
an anode housed within the housing and proximate the open distal end of the housing, and
a magnetic field having magnetic field lines positioned about the external cathode-insulator interface at an incidence angle of about 20 degrees to about 30 degrees relative to the external cathode-insulator interface,

wherein when the power unit supplies power to the thruster assembly, a plasma is produced about the external cathode-insulator interface and directed distally by the magnetic field.

14. The micro-cathode thruster of claim 13 , wherein the anode is a tubular anode or a cylindrical anode.

15. The micro-cathode thruster of claim 13 , wherein the cathode has a longitudinal axis and the magnetic field has magnetic field lines oriented at an incidence angle of about 20 degrees to about 30 degrees relative to the longitudinal axis of the cathode about the external cathode-insulator interface.

16. The micro-cathode thruster of claim 13 , wherein the magnetic field lines are oriented about 30 degrees relative to the external cathode-insulator interface.

17. The micro-cathode thruster of claim 13 , wherein the housing includes an abutment proximate the open distal end for arresting movement of the cathode in a distal direction.

18. A method of enhancing the thrust-to-power ratio of a micro-cathode thruster comprising:
providing a vacuum arc thruster that includes:
a tubular housing having an open distal end,
a tubular cathode housed within the housing, the cathode having a distal end proximate the open distal end of the housing,
an insulator in contact with the cathode forming an external cathode-insulator interface, and
an anode housed within the housing and proximate the open distal end of the housing; and

generating a magnetic field positioned about the external cathode-insulator interface and having magnetic field lines angled at an incidence angle of about 20 degrees to about 30 degrees relative to the external cathode-insulator interface.

19. A method of controlling thruster output of a micro-cathode thruster comprising:
the method of claim 18 further comprising providing a controller that controls the magnetic field strength of the magnetic field.

Assignees

• Univ George Washington

Inventors

• Keidar Michael
• Shashurin Alexey
• Zhuang Tai Sen

Classifications

• F03H1/0087 Primary

  Electro-dynamic thrusters, e.g. pulsed plasma thrusters · CPC title

• B64G1/413

  Ion or plasma engines · CPC title

• B64G1/405 Primary

  Operations & Transport · mapped topic

• H05H1/50

  and using applied magnetic fields, e.g. for focusing or rotating the arc · CPC title

• F03H1/0081

  Electromagnetic plasma thrusters · CPC title