NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
PT-1 Plasmoid Thruster Capable of Multi-Mode OperationThis slide presentation reviews the concept of a Plasmoid Thruster that is capable of operating in several different modes. A plasmoid is a compact plasma structure with an integral magnetic field, that may be categorized according to the relative strength of the poloidal and toroidal magnetic fields. A plasmoid thruster would operate by repetitively producing plasmoids that are accelerated to high velocity. The process is inductive, and the magnetic structure of the plasmoid suppresses thermal and mass losses, and improves detachment of the exhaust. The Drive and Bias circuits, the gas distribution, the pre-ionization stage, and the operation sequence are detailed. The advantages of the Plasmoid thruster and the research and technology required for development of this form of propulsion is reviewed.
Document ID
20110004350
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
Authors
Miller, Robert
(Radiance Technologies, Inc. Huntsville, AL, United States)
Rose, Frank
(Radiance Technologies, Inc. Huntsville, AL, United States)
Eskridge, Richard
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Martin, Adam
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Alam, Mohammed
(University of South Alabama Mobile, AL, United States)
Date Acquired
August 25, 2013
Publication Date
October 28, 2008
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
M09-0162
Report Number: M09-0162
Meeting Information
Meeting: 17th Advanced Space Propulsion Workshop (ASPW 2008)
Location: Pasadena, CA
Country: United States
Start Date: October 28, 2008
End Date: October 30, 2008
Sponsors: Jet Propulsion Lab., California Inst. of Tech., Air Force Research Lab.
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available