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Title AN INVESTIGATION OF HALL PROPULSOR CHARACTERISTICS
Creator/Author Brandmaier, H.E. ; Durand, J.L. ; Gourdine, M.C. ; Rubels, A.
Publication Date1964 Apr 01
OSTI IdentifierOSTI ID: 4004760
Resource TypeJournal Article
Resource RelationAIAA (Am. Inst. Aeron. Astronaut.) J.; Vol: 2
Research OrgCurtiss-Wright Corp., Wood-Ridge, N.J.
SubjectPHYSICS; ACCELERATION; BIBLIOGRAPHY; CONFIGURATION; DIFFERENTIAL EQUATIONS; ELECTRIC FIELDS; FABRICATION; FLUID FLOW; FREQUENCY; HALL EFFECT; IONIZATION; IONS; MACH NUMBER; MAGNETIC FIELDS; MAGNETOHYDRODYNAMICS; PLANNING; PLASMA; PROPULSION; RADIO WAVES; TEMPERATURE; ULTRASONICS; VELOCITY; VISCOSITY
Description/Abstract 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.
LanguageEnglish
FormatPages: 674-81
System Entry Date2001 Jun 03

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