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Pulsed Electromagnetic Acceleration of PlasmasA major shift in paradigm in driving pulsed plasma thruster is necessary if the original goal of accelerating a plasma sheet efficiently to high velocities as a plasma "slug" is to be realized. Firstly, the plasma interior needs to be highly collisional so that it can be dammed by the plasma edge layer not (upstream) adjacent to the driving 'vacuum' magnetic field. Secondly, the plasma edge layer needs to be strongly magnetized so that its Hall parameter is of the order of unity in this region to ensure excellent coupling of the Lorentz force to the plasma. Thirdly, to prevent and/or suppress the occurrence of secondary arcs or restrike behind the plasma, the region behind the plasma needs to be collisionless and extremely magnetized with sufficiently large Hall parameter. This places a vacuum requirement on the bore conditions prior to the shot. These requirements are quantified in the paper and lead to the introduction of three new design parameters corresponding to these three plasma requirements. The first parameter, labeled in the paper as gamma (sub 1), pertains to the permissible ratio of the diffusive excursion of the plasma during the course of the acceleration to the plasma longitudinal dimension. The second parameter is the required Hall parameter of the edge plasma region, and the third parameter the required Hall parameter of the region behind the plasma. Experimental research is required to quantify the values of these design parameters. Based upon fundamental theory of the transport processes in plasma, some theoretical guidance on the choice of these parameters are provided to help designing the necessary experiments to acquire these data.
Document ID
20030002753
Acquisition Source
Marshall Space Flight Center
Document Type
Other
Authors
Thio, Y. C. Francis
(NASA Marshall Space Flight Center Huntsville, AL United States)
Cassibry, Jason T.
(Alabama Univ. Huntsville, AL United States)
Markusic, Tom E.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Rodgers, Stephen L.
Date Acquired
September 7, 2013
Publication Date
January 1, 2002
Subject Category
Plasma Physics
Report/Patent Number
AIAA Paper 2002-3803
Report Number: AIAA Paper 2002-3803
Meeting Information
Meeting: 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Location: Indianapolis, IN
Country: United States
Start Date: July 7, 2002
End Date: July 10, 2002
Sponsors: Society of Automotive Engineers, Inc., American Society of Mechanical Engineers, American Inst. of Aeronautics and Astronautics, American Society for Electrical Engineers
Distribution Limits
Public
Copyright
Public Use Permitted.
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