An investigation of hall propulsor characteristics

An investigation of hall propulsor characteristics

The steady, one-dimensional, inviscid magnetogasdynamic flow equations are derived for the coaxial, constant area, Hall propulsor using a slightly ionized plasma. For the case of a radial magnetic field and axial electric field, flow regimes are established for which supersonic acceleration combined...

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Veröffentlicht in:AIAA journal 1964-04, Vol.2 (4), p.674-681
Hauptverfasser: BRANDMAIER, H. E, DURAND, J. L, GOURDINE, M. C, RUBEL, A
Format: Artikel
Sprache:eng
Schlagworte:
ACCELERATION
BIBLIOGRAPHY
CONFIGURATION
DIFFERENTIAL EQUATIONS
ELECTRIC FIELDS
FABRICATION
FLUID FLOW
FREQUENCY
HALL EFFECT
IONIZATION
IONS
MACH NUMBER
MAGNETIC FIELDS
MAGNETOHYDRODYNAMICS
PHYSICS
PLANNING
PLASMA
PROPULSION
RADIO WAVES
TEMPERATURE
ULTRASONICS
VELOCITY
VISCOSITY
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Beschreibung
Zusammenfassung:The steady, one-dimensional, inviscid magnetogasdynamic flow equations are derived for the coaxial, constant area, Hall propulsor using a slightly ionized plasma. For the case of a radial magnetic field and axial electric field, flow regimes are established for which supersonic acceleration combined with an increasing axial Mach number is PLEASE DELETE ABSTRACT 21391.
ISSN:0001-1452
1533-385X
DOI:10.2514/3.2402