Effect of surface roughness on secondary electron emission in a Hall discharge

Collection of Technical Papers - AIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference

Volumn 5, Issue , 2006, Pages 3399-3407

  Taccogna, F ^a,c,d   Schneider, R ^a,e   Longo, S ^b,d,f   Capitelli, M ^b,d,f  

^a MAX PLANCK INSTITUT FÜR PLASMAPHYSIK   (Germany)

^b UNIVERSITY OF BARI   (Italy)

^c Edge Phys Div   (Germany)

^d AIAA   (United States)

^e Helmholtz Association Junior Research Group 'Computational Material Science'   (Germany)

^f Chemistry Dept   (Italy)

Author keywords

[No Author keywords available]

Indexed keywords

DIELECTRIC WALLS; HALL DISCHARGE; HALL THRUSTER; LOCAL FIELD APPROXIMATION;

ACCELERATION; COMPUTER SIMULATION; DIELECTRIC MATERIALS; ELECTRON EMISSION; HALL EFFECT; SURFACE ROUGHNESS;

AIRCRAFT PROPULSION;

EID: 34249104163     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (18)

1. Ahedo, E.,"Presheath/Sheath model with secondary electron emission from two parallel walls", Phys. Plasmas, Vol. 9, No. 10, 2002, pp. 4340-4347.
2. Keidar, M., Boyd, I. D., Beilis, I.I., "Plasma flow and plasma-wall transition in Hall thruster channel", Phys. Plasmas, Vol. 8, No. 12, 2001, pp. 5315-5322.
3. Pandey, B. P., Roy, S., "Sheath in the presence of secondary electron emission and sputtering yield", 36th AIAA Thermophysics Conference, AIAA-2003-10358, Orlando, Florida, 2003.
4. Barral, S., Makowski, K., Peradzyriski, Z., Gascon, N., Dudeck, M., "Wall material effects in stationary plasma thrusters. II. Near-wall and in-wall conductivity", Phys. Plasmas, Vol. 10, No. 10, 2003, pp. 4137-4152.
5. Ahedo, E., Parra, F. I., "Partial trapping of secondary-electron emission in a Hall thruster plasma", Phys. Plasmas, Vol. 12, 073503, 2005.
6. Jolivet, L., Roussel, J.-F., 3rd Spacecraft Propulsion Conference, SP-465, Cannes. France, European Space Agency, Noordwijk, The Netherlands, 2000, p. 367.
7. Morozov, A. I., Savel'ev, V. V., "One-dimensional model of the Debye layer near a dielectric surface", Plasma Phys. Rep., Vol. 28, No. 12, 2002, pp. 1017-1023.
8. Sydorenko, D., Smolyakov, A., Kaganovich, I., Raitses, Y., "Kinetic simulation of secondary electron emission effects in Hall thrusters", Phys. Plasmas, Vol. 13, 014501, 2006.
9. Eastwood, J. W., Hockney, R. W., Computer Simulation using Particle, McGraw-Hill, New York, 1981.
10. Birdsall, C. K., Langdon, A. B., Plasma Physics via Computer Simulation, McGraw-Hill, New York, 1985.
11. Nanbu, K., "Probability theory of electron-molecule, ion-molecule, molecule-molecule, and coulomb collisions for particle modeling of materials processing plasmas and gases", IEEE Trans. Plasma Sci., Vol 28, No. 3, 2000, pp. 971-.990.
12. Szabo, J. J. Jr., "Fully kinetic numerical modeling of a plasma thruster", PhD Dissertation, Aeronautics and Astronautics Dept., Massachusetts Institute of Technology, Boston, New England, 2001.
13. Nanbu, K., Kitatani, Y., "An ion-neutral species collision model for particle simulation of glow discharge", J. Phys. D: Appl. Phys., Vol. 28, 1995, pp. 324-330.
14. Furman, M. A., Pivi, M. T. F., "Probabilistic model for the simulation of secondary electron emission", Phys. Rev. Special Topics-Accel. and Beams, Vol. 5, 124404, 2002.
15. Taccogna, F., Longo, S., Capitelli, M., "Plasma sheaths in Hall discharge", Phys. Plasmas, Vol. 12, 093506, 2005.
16. D. R. Yu, Z. W. Wu, X. G. Wang, "Numerical simulation for near wall conductivity effect on current profile in the annular channel of Hall-type stationary plasma thrusters", Phys. Plasmas, Vol. 12, 043507, 2005.
17. Taccogna, F., Longo, S., Capitelli, M., "Particle-in-Cell with Test-Particle Monte Carlo (PIC-TPMC) simulation of SPT-100 exhaust plumes", J. Spac &. Rock., Vol. 39, No. 3, 2002, pp. 409-419.
18. Taccogna, F., Longo, S., Capitelli, M., "Very-near-field plume simulation of a stationary plasma thruster", J. Europ. Phys.-Appl. Phys., Vol. 28, 2004, pp. 113-122.