Systems and methods for cylindrical hall thrusters with independently controllable ionization and acceleration stages
Abstract
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.
- Inventors:
- Issue Date:
- Research Org.:
- Princeton Plasma Physics Laboratory (PPPL), Princeton, NJ (United States)
- Sponsoring Org.:
- USDOE
- OSTI Identifier:
- 1130972
- Patent Number(s):
- 8723422
- Application Number:
- 13/035,475
- Assignee:
- The Aerospace Corporation (El Segundo, CA); Trustees of Princeton University (Princeton, NJ)
- Patent Classifications (CPCs):
-
F - MECHANICAL ENGINEERING F03 - MACHINES OR ENGINES FOR LIQUIDS F03H - PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
H - ELECTRICITY H01 - BASIC ELECTRIC ELEMENTS H01J - ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
- DOE Contract Number:
- ACO2-09CH11466
- Resource Type:
- Patent
- Resource Relation:
- Patent File Date: 2011 Feb 25
- Country of Publication:
- United States
- Language:
- English
- Subject:
- 42 ENGINEERING
Citation Formats
Diamant, Kevin David, Raitses, Yevgeny, and Fisch, Nathaniel Joseph. Systems and methods for cylindrical hall thrusters with independently controllable ionization and acceleration stages. United States: N. p., 2014.
Web.
Diamant, Kevin David, Raitses, Yevgeny, & Fisch, Nathaniel Joseph. Systems and methods for cylindrical hall thrusters with independently controllable ionization and acceleration stages. United States.
Diamant, Kevin David, Raitses, Yevgeny, and Fisch, Nathaniel Joseph. Tue .
"Systems and methods for cylindrical hall thrusters with independently controllable ionization and acceleration stages". United States. https://www.osti.gov/servlets/purl/1130972.
@article{osti_1130972,
title = {Systems and methods for cylindrical hall thrusters with independently controllable ionization and acceleration stages},
author = {Diamant, Kevin David and Raitses, Yevgeny and Fisch, Nathaniel Joseph},
abstractNote = {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.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2014},
month = {5}
}
Save to My Library
You must Sign In or Create an Account in order to save documents to your library.
Works referenced in this record:
Plasma accelerator of short length with closed electron drift
patent, December 1995
- Valentian, Dominique; Morozov, Alexei; Bougrova, Antonina
- US Patent Document 5,475,354
Cylindrical geometry hall thruster
patent, September 2002
- Raitses, Yevgeny; Fisch, Nathaniel J.
- US Patent Document 6,448,721
Segmented electrode hall thruster with reduced plume
patent, August 2004
- Fisch, Nathaniel J.; Raitses, Yevgeny
- US Patent Document 6,777,862
Cylindrical geometry hall thruster
patent-application, February 2002
- Raitses, Yevgeny; Fisch, Nathaniel J.
- US Patent Application 09/834397; 20020014845
Combined radio frequency and hall effect ion source and plasma accelerator system
patent-application, December 2006
- Hruby, Vladimir; Hohman, Kurt; Brogan, Thomas
- US Patent Application 11/412619; 20060284562
Two-stage hall effect plasma accelerator including plasma source driven by high-frequency discharge
patent-application, December 2006
- Kuninaka, Hitoshi
- US Patent Application 11/141189; 20060290287
Experimental and theoretical studies of cylindrical Hall thrusters
journal, May 2007
- Smirnov, Artem; Raitses, Yegeny; Fisch, Nathaniel J.
- Physics of Plasmas, Vol. 14, Issue 5
Magnetic Field Effects on the Plume of a Diverging Cusped-Field Thruster
conference, November 2012
- Matlock, Taylor; Gildea, Stephen; Hu, Fuzhou
- 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit