This article has multiple issues. Please helpimprove it or discuss these issues on thetalk page.(Learn how and when to remove these messages) (Learn how and when to remove this message)
|
Theelectrodeless plasma thruster is aspacecraft propulsion engine commercialized under the acronym "E-IMPAcT" for "Electrodeless-Ionization Magnetized Ponderomotive Acceleration Thruster". It was created byGregory Emsellem, based on technology developed by FrenchAtomic Energy Commission scientist DrRichard Geller and Dr.Terenzio Consoli, for high speedplasma beam production.
Theelectrodelessplasma thruster was developed and adapted to various spacecraft propulsion needs byThe Elwing Company between 2002 and 2015.
This thruster technology can deliver large thrust density as the acceleration process is not limited by plasma density throughHall Parameter or grid electrical screening. Further, as the ponderomotive force accelerates all plasma species in the same direction, this thruster technology does not need anyneutralizer. The fact that electrodeless plasma thruster is inherently multi-staged allows it to optimize both stages independently, or to throttle the thruster at constant power between higherspecific impulse and higherthrust. The field of ponderomotive force is created by a non-uniform high frequency field and static magnetic field, thus it implies no grids nor contact between the plasma and any electrodes, hence it avoids most thruster erosion and spacecraft contamination issues.
Propulsion systems based on electrodeless plasma thrusters seem ideally suited for orbit raising for largegeostationary satellites, and would also be able to performorbital stationkeeping, hence enabling important propellant mass savings. The ability of this technology to provide large thrust density also allows faster missions to the outer planets.
The use ofponderomotive force to accelerate a plasma has recently been investigated from a theoretical point of view byPrinceton Plasma Physics Laboratory scientists I. Y. Dodin, Y. Raitses and N. J. Fisch.[2]
Some theoretical research has also been reported around the debated issue of the existence of adouble layer in such a thruster, even if such a double layer structure would be current-free, as both ions and electrons travel in the same direction at the same average terminal speed. The existence of current free double layer is still debated among plasma physicists.