Air-breathing plasma thruster

Patent metadata

Field	Value
Publication number	US-12479604-B2
Application number	US-202519093578-A
Country	US
Kind code	B2
Filing date	Mar 28, 2025
Priority date	Sep 29, 2023
Publication date	Nov 25, 2025
Grant date	Nov 25, 2025

Abstract

One or more embodiments relates to an air-breathing plasma thruster including a thruster wall, an anode, a cathode, and at least one ring electrode. The thruster wall defines a cylindrical channel, the cylindrical channel having a first end and an opposing second end in fluid communication with the first end, where the cylindrical channel is adapted to receive incoming airflow. The anode is at the first end of the channel and the cathode is at the second end of the channel opposite the first end. The at least one ring electrode is positioned on the thruster wall.

First claim

What is claimed is:

1 . A method of forming a plasma jet using an air-breathing plasma thruster, the method comprising:
receiving incoming airflow in a cylindrical channel defined by an inside wall of the air-breathing thruster, forming a volume of air; ionizing the volume of air using electron beams generated by one or more cathodes and confined by segmented electrodes and one or more magnetic field cusps, forming ionized air; accelerating the ionized air using applied electric and diverging magnetic fields, forming a plasma jet; and generating the plasma jet at an outlet of the air-breathing thruster.

2 . The method of forming the plasma jet of claim 1 further including forming an electric field and injecting energy into the cylindrical channel, enabling confining the electron beams and sustaining the ionization of the volume of air.

3 . The method of forming the plasma jet of claim 2 further including applying a voltage to the segmented electrodes, forming the electric field and injecting the energy into the cylindrical channel.

4 . The method of forming the plasma jet of claim 1 wherein at least one of the segmented electrodes is an electron-emitting electrode.

5 . The method of forming the plasma jet of claim 4 further comprises injecting electrons into the cylindrical channel using the electron-emitting electrode.

6 . The method of forming the plasma jet of claim 1 wherein at least one of the segmented electrodes is biased positive and another of the segmented electrodes is biased negative with respect to the positive biased segmented electrode.

7 . The method of forming the plasma jet of claim 1 further including moving the air-breathing plasma thruster in a direction opposite the plasma jet.

8 . A method of forming a plasma jet using an air-breathing plasma thruster, the method comprising:
forming a volume of air in a cylindrical channel of the air-breathing thruster; ionizing the volume of air using electron beams generated by cathodes and confined by segmented electrodes including at least one electron-emitting electrode, and one or more magnetic field cusps, forming ionized air; accelerating the ionized air using applied electric and diverging magnetic fields, forming a plasma jet; and generating the plasma jet at an outlet of the air-breathing thruster.

9 . The method of forming the plasma jet of claim 8 further including receiving incoming airflow in a cylindrical channel defined by an inside wall of the air-breathing thruster, forming the volume of air.

10 . The method of forming the plasma jet of claim 8 further comprising injecting electrons into the cylindrical channel using the electron-emitting electrode.

11 . The method of forming the plasma jet of claim 8 wherein at least one of the electron-emitting electrode comprises a plurality of ring electrodes and further including applying a voltage to the plurality of ring electrodes, forming the electric field and injecting energy, confining the electron beams and sustaining the ionization of the volume of air.

12 . The method of forming the plasma jet of claim 8 further including accelerating the ionized air using applied electric and diverging magnetic fields, forming the plasma jet.

13 . The method of forming the plasma jet of claim 8 further including moving the air-breathing plasma thruster in a direction opposite the plasma jet.

14 . A method of forming a plasma jet using an air-breathing plasma thruster, the method comprising:
forming a volume of air in a cylindrical channel of the air-breathing thruster; ionizing the volume of air using electron beams generated by cathodes and confined by segmented electrodes and one or more magnetic field cusps, forming ionized air, wherein at least one of the segmented electrodes is biased positive and another of the segmented electrodes is biased negative with respect to the positive biased segmented electrode; accelerating the ionized air using applied electric and diverging magnetic fields, forming a plasma jet; and generating the plasma jet at an outlet of the air-breathing thruster.

15 . The method of forming the plasma jet of claim 14 further including receiving incoming airflow in the cylindrical channel defined by an inside wall of the air-breathing thruster, forming the volume of air.

16 . The method of forming the plasma jet of claim 14 wherein the segmented electrodes comprise a plurality of ring electrodes and further including applying a voltage to the plurality of ring electrodes, forming the electric field and injecting energy, confining the electron beams and sustaining the ionization of the volume of air.

17 . The method of forming the plasma jet of claim 14 further including accelerating the ionized air using applied electric and diverging magnetic fields, forming the plasma jet.

18 . The method of forming the plasma jet of claim 14 further including moving the air-breathing plasma thruster in a direction opposite the plasma jet.

Assignees

• Us Energy
• Us Dept Energy

Inventors

• Raitses Yevgeny

Classifications

• F03H1/0068

  with a central channel, e.g. end-Hall type · CPC title

• B64G1/411

  Electric propulsion · CPC title

• F03H1/0093

  Electro-thermal plasma thrusters, i.e. thrusters heating the particles in a plasma (resistojets per se B64G1/415) · CPC title

• F03H1/0087

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

• F03H1/0081

  Electromagnetic plasma thrusters · CPC title