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Electricity / Electrodes / Ion thruster / Ions / Plasma physics / Magnetoplasmadynamic thruster / Anode / Cathode / Space charge / Electromagnetism / Spacecraft propulsion / Physics


Abstract An array of diagnostic techniques was used to study anode phenomena in quasisteady self-field MPD thrusters operated at power levels between 150 kW and 7 MW with argon and helium propellants. Spatially resolved
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Document Date: 2004-04-21 00:44:01


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File Size: 1,59 MB

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Country

Soviet Union / /

IndustryTerm

propellant gas / Chemical rockets / energy addition / chemical reactions / low power device / exotic systems / multi-megawatt quasi-steady devices / chemical energy / non-liquid metal propellants / random thermal energy / oil / kinetic energy / ambient gas / internal chemical reactions / intrinsic energy / quasi-steady device / powered devices / steady-state devices / random electron thermal energy / gas enthalpy / thruster technology / electrical energy / energy / gas stream / directed kinetic energy / anode energy transfer / /

Organization

Lorentz Force / /

Technology

Radiation / heat transfer / MPD thruster technology / /

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