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Current driven instabilities of an electromagnetically accelerated plasmaA plasma instability that strongly influences the efficiency and lifetime of electromagnetic plasma accelerators was quantitatively measured. Experimental measurements of dispersion relations (wave phase velocities), spatial growth rates, and stability boundaries are reported. The measured critical wave parameters are in excellent agreement with theoretical instability boundary predictions. The instability is current driven and affects a wide spectrum of longitudinal (electrostatic) oscillations. Current driven instabilities, which are intrinsic to the high-current-carrying magnetized plasma of the magnetoplasmadynmic (MPD) accelerator, were investigated with a kinetic theoretical model based on first principles. Analytical limits of the appropriate dispersion relation yield unstable ion acoustic waves for T(i)/T(e) much less than 1 and electron acoustic waves for T(i)/T(e) much greater than 1. The resulting set of nonlinear equations for the case of T(i)/T(e) = 1, of most interest to the MPD thruster Plasma Wave Experiment, was numerically solved to yield a multiparameter set of stability boundaries. Under certain conditions, marginally stable waves traveling almost perpendicular to the magnetic field would travel at a velocity equal to that of the electron current. Such waves were termed current waves. Unstable current waves near the upper stability boundary were observed experimentally and are in accordance with theoretical predictions. This provides unambiguous proof of the existence of such instabilites in electromagnetic plasma accelerators.
Document ID
19890018365
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chouetri, E. Y.
(Princeton Univ. NJ, United States)
Kelly, A. J.
(Princeton Univ. NJ, United States)
Jahn, R. G.
(Princeton Univ. NJ, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1988
Publication Information
Publication: DGLR, DGLR(AIAA)JSASS 20th International Electric Propulsion Conference: Proceedings
Subject Category
Spacecraft Propulsion And Power
Accession Number
89N27736
Funding Number(s)
CONTRACT_GRANT: NAS9-54997
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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