MPD thruster performance using pure gases and mixtures as propellant

Author:

Paganucci Fabrizio,Andrenucci Mariano

Publisher

American Institute of Aeronautics and Astronautics

Reference5 articles.

1. 'R.J.Jahn."PhysicsofElectricPropulsion",McGrawHill, NewYork. 1966.

2. H.R. Kaufman, R.S. Robinson, "Electric Thruster Performance forOrbitW i gandManeuvering",AIAA-82-1247, 18th Joint Propulsion Conference, Cleveland. Ohio, June 21-23.1982. ' C.Selph.D.Perkins,"AnAnalysisofElectromagnetic Thrusters forOrbitRaising",IEPC-84-80,17thInternational ElectricPropulsionConference, Tokio.1984. ' L.K.Rudolph,"DesignandBenefitsofPulsedMPD Thruster Orbit Transfer Vehicles". IEPC-84-81. 17th InternationalElectricPropulsionConference, Tokio,1984. ' L.K.Rudolph,G.M.Ogg,"OrbitTransferUsingHigh PowerMPDThrus(ers",AIAA-85-1478,21stJointPropulsion Conference,Monterey,CA.July8-10.1985.

3. The manifestation of Alfven's hypothesis of critical ionization velocity in the performance of MPD thrusters

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