3-D Computation of Plasma Thruster Plumes

Author:

Passaro Andrea1,Vicini Alessandro2,Biagioni Leonardo2

Affiliation:

1. Aerospace Division - CPR

2. Alta S.p.A.

Publisher

American Institute of Aeronautics and Astronautics

Reference15 articles.

1. Bird,G.A.,MolecularGasDynamicsandtheDirectSimulationofGasFlows,OxfordSciencePublications,Oxford,1994.

2. Birdsall,C.K.,Langdon,A.B.,PlasmaPhysicsViaComputerSimulation,McGraw-Hill,NewYork,1985.

3. Hockney,R.W.,Eastwood,J.W.,ComputerSimulationUsingParticles,McGraw-Hill,NewYork,1981.

4. Andrenucci, M., Biagioni, L., Passaro, A. "PIC/DSMC Models for Hall Effect Thruster Plumes: Present Status and Ways Forward", AIAAPaper 2002-4254, July2002.

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1. Kinetic electron model for plasma thruster plumes;Plasma Sources Science and Technology;2018-03-27

2. Space Debris Removal with an Ion Beam Shepherd Satellite: target-plasma interaction;47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2011-07-31

3. Numerical Rebuilding of SMART-1 Hall Effect Thruster Plasma Plume;Journal of Propulsion and Power;2010-01

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