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The Plasmoid Thruster Experiment (PTX)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. If B(sub p/B(sub t) much greater than 1 it is an FRC; if B(sub p) approximately equal to B(sub t), it is a Spheromak. 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, This concept should be capable of producing an Isp in the range of 5,000 - l0,000 seconds, with high thrust density. PTX is a device designed to study this concept. The plasmoid is formed inside of a single turn conical theta-pinch coil, driven by a 560 nF, 35 kV capacitor bank. Experiments conducted with a static-fill of propellant gas (6% H2 in He) demonstrated liable ionization over a pressure range of 40 - 200 mTorr. A fast gas-puff valve to inject propellant has since been added, and a ringing preionization circuit to independently control ionization has been tested, hydrogen, deuterium, argon, and an N2 / H2 mixture have been tried as propellants. Measurements of the plasmoid shape, mass, and velocity, using a variety of diagnostics will be presented.
Document ID
20050092325
Acquisition Source
Marshall Space Flight Center
Document Type
Abstract
Authors
Martin, Adam
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Eskridge, Richard
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Lee, Mike
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Fimohnsti, Peter
(Alabama Univ. Huntsville, AL, United States)
Koelfgen, Syri J.
(Alabama Univ. Huntsville, AL, United States)
Date Acquired
August 22, 2013
Publication Date
January 1, 2005
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: 46th Annual Meeting of the Division of Plasma Physics
Location: Savannah
Country: United States
Start Date: November 15, 2004
End Date: November 19, 2004
Distribution Limits
Public
Copyright
Other

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