Modeling and Analysis of a Megawatt-Class Magnetoplasmadynamic Thruster

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23 Scopus citations

Abstract

The magnetohydrodynamic code MACH2 is utilized to investigate the operation and performance of a megawatt-class, quasi-steady, self-field magnetoplasmadynamic thruster. The numerical results are validated by comparisons to experimental data and offer significant insights into this regime of operation. Specifically, operation at 0.5-6 MW and 1.37 g/s shows incomplete hydrogen-propellant ionization that is dominated by electron-neutral collisions, which in turn increase the plasma voltage, but do not substantially increase thrust. Acceleration is of a hybrid nature, transitioning from primarily electrothermal to predominantly electromagnetic with increasing current level. Detailed interrogation of energy deposition shows significant deposition to internal modes, as opposed to external-circuit-element losses and electrode losses via fall voltage and thermal conduction, even at the higher power levels. These frozen-flow and radial-momentum losses can be reduced while the system still operates with minimum power penalty by proper expansion of the flow.

Original languageEnglish (US)
Pages (from-to)204-210
Number of pages7
JournalJournal of Propulsion and Power
Volume20
Issue number2
DOIs
StatePublished - 2004

ASJC Scopus subject areas

  • Aerospace Engineering
  • Fuel Technology
  • Mechanical Engineering
  • Space and Planetary Science

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