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Incorporation of an Energy Equation into a Pulsed Inductive Thruster Performance ModelA model for pulsed inductive plasma acceleration containing an energy equation to account for the various sources and sinks in such devices is presented. The model consists of a set of circuit equations coupled to an equation of motion and energy equation for the plasma. The latter two equations are obtained for the plasma current sheet by treating it as a one-element finite volume, integrating the equations over that volume, and then matching known terms or quantities already calculated in the model to the resulting current sheet-averaged terms in the equations. Calculations showing the time-evolution of the various sources and sinks in the system are presented to demonstrate the efficacy of the model, with two separate resistivity models employed to show an example of how the plasma transport properties can affect the calculation. While neither resistivity model is fully accurate, the demonstration shows that it is possible within this modeling framework to time-accurately update various plasma parameters.
Document ID
20120001445
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Polzin, Kurt A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Reneau, Jarred P.
(Mississippi State Univ. Starkville, MS, United States)
Sankaran, Kameshwaran
(Whitworth Univ. Spokane, WA, United States)
Date Acquired
August 25, 2013
Publication Date
September 11, 2011
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
M11-1025
M11-1022
IEPC Paper 2011-181
M11-0500
Report Number: M11-1025
Report Number: M11-1022
Report Number: IEPC Paper 2011-181
Report Number: M11-0500
Meeting Information
Meeting: 32nd International Electric Propulsion Conference
Location: Wiesbaden
Country: Germany
Start Date: September 11, 2011
End Date: September 15, 2011
Sponsors: Electric Rocket Propulsion Society
Distribution Limits
Public
Copyright
Public Use Permitted.
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