IP Library › Granted Patent US 11,486,371
Granted Patent B2
US 11,486,371 · App. 16/771,026 · Granted Nov 1, 2022

Hall thruster with annular cathode

Inventor: Justin Pucci (Bothell, WA)
Assignee: AEROJET ROCKETDYNE, INC.
F03H1/0037
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 11,486,371
App. No.
16/771,026
Granted
Nov 1, 2022
Kind
B2
Abstract

A Hall thruster includes an annular discharge region and an annular cathode concentric to the annular discharge region.

Claims (20)

1. A Hall thruster comprising:

a magnetic pole disposed about a central axis;

a passage along the central axis through the magnetic pole;

an annular discharge region;

an anode, wherein at least a portion of the anode is disposed in the annular discharge region; and

an annular cathode in the form of a ring concentric to the annular discharge region around the central axis, wherein the annular cathode is radially inwardly displaced from the annular discharge region and radially outwardly displaced from the passage.

2. The Hall thruster as recited in claim 1 , wherein the annular cathode is circumscribed by the annular discharge region.

3. The Hall thruster as recited in claim 1 , further comprising another portion of the anode surrounding the annular discharge region.

4. The Hall thruster as recited in claim 1 , wherein the annular cathode is circumscribed by the annular discharge region.

5. The Hall thruster as recited in claim 1 , wherein a radially outer surface of the ring is substantially equidistant from the discharge region.

6. The Hall thruster as recited in claim 1 , wherein the anode and the annular cathode are electrically coupled to generate an electric field there between and induce electrons to drift into the annular discharge region.

7. A Hall thruster comprising:

a radially inner magnetic pole and a radially outer magnetic pole, wherein the radially inner magnetic pole and the radially outer magnetic pole are disposed about a central axis;

a passage along the central axis through the radially inner magnetic pole;

an annular discharge region between the radially inner magnetic pole and the radially outer magnetic pole;

a propellant gas feeder operable to feed propellant gas to the annular discharge region;

an annular cathode in the form of a ring concentric to the annular discharge region around the central axis, wherein the annular cathode is radially inwardly displaced from the annular discharge region and radially outwardly displaced from the passage;

an anode disposed in the annular discharge region; and

at least one magnet magnetically coupled with the radially inner magnetic pole and the radially outer magnetic pole to generate a magnetic field across the annular discharge region.

8. The Hall thruster as recited in claim 7 , wherein the annular cathode is circumscribed by the annular discharge region.

Assignments (4)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 27, 2026
From: L3HARRIS TECHNOLOGIES, INC.; AEROJET ROCKETDYNE, INC.; AEROJET ROCKETDYNE OF DE, INC.; L3HARRIS CINCINNATI ELECTRONICS CORPORATION
To: ROCKETFORCE TECHNOLOGIES LLC
Reel/Frame 076068/0283 →
TERMINATION AND RELEASE OF SECURITY INTEREST IN PATENTS Recorded Jul 28, 2023
From: BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT
To: AEROJET ROCKETDYNE, INC.
Reel/Frame 064423/0966 →
NOTICE OF GRANT OF SECURITY INTEREST IN PATENTS Recorded Sep 28, 2022
From: AEROJET ROCKETDYNE, INC.
To: BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT
Reel/Frame 061561/0451 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 9, 2020
From: PUCCI, JUSTIN
To: AEROJET ROCKETDYNE, INC.
Reel/Frame 052878/0511 →
Continuity (1)
Related Publication 20210164453A1 · Jun 3, 2021