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[3] Jahn, R.G., “Physics of electric propulsion”, 1968, McGraw-Hill Company, New- York

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Bibliografia

209

BIBLIOGRAFIA

[1] Cornelisse,J.W. et al., “Rocket propulsion and spacecraft dynamics” Pitman, London 1978.

[2] Sutton G.P., “Rocket propulsion of elements VI Ed.”, John Wiley & sons, New York, 1992.

[3] Jahn, R.G., “Physics of electric propulsion”, 1968, McGraw-Hill Company, New- York.

[4] Choueiri, E.Y. “ A critical History of Electric Propulsion: The First 50 Years (1906- 1956)”, Journal of Propulsion and Power, Vol.20, N°2, 2004.

[5] Andrenucci M.,”Dispense del corso di Propulsione Aerospaziale”, 2006-2007, Dipartimento di ingegneria Aerospaziale, Pisa.

[6] D’Agostino L., “Dispense del corso di Endoreattori”, 2006-2007, Dipartimento di Ingegneria Aerospaziale, Pisa.

[7] Vladimir Kim, Konstantin Kozubsky, Vyacheslav Murashko and Veniamin Semenkin, “History of the Hall thrusters development in USSR”, IEPC -2007- 142, 30th International Electric Propulsion Conference, Florence, 2007.

[8] Richard Fitzpatrick, “Introduction to Plasma Physics”, Institute for Fusion Studies University of Texas at Austin, 1998.

[9] Piliero, Battista. “Leggi di scala e criteri di dimensionamento dei propulsori a effetto Hall” Tesi di laurea in Ingegneria Aerospaziale, Università di Pisa.

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Bibliografia

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[10] Peter Y. Peterson, Alec D. Gallimore§, and James M. Haas, “Experimental Investigation of a Hall Thruster Internal Magnetic Field Topography”, IEPC 01-030, 27th International Electric Propulsion Conference, Pasadena, CA, October 15-19, 2001.

[11] E. Ahedo, P. Martınez-Cerezo, and M. Martınez-Sanchez,”One-dimensional model of the plasma flow in a Hall Thruster” Phys. Plasmas 8, 3058 (2001)

[12] Ahedo, E., Gallardo, J.M. and Martinez-Sanchez, M., ”Effects of the radial wall interaction on the Hall thruster discharge,” Physics of Plasmas, Vol.10, N°8, 2003.

[13] Barral, S., Makowski, K., Peradzyinski Z., Gascon N., Dudeck M., “ Wall material effects in stationary plasma thrusters, near wall and in wall conductivity,” Physics of Plasmas ,Vol.10, 2003.

[14] Roy D. and Pandey B.P., “Modeling the effect of plasma-wall interaction in a Hall thruster”, AIAA 2003-0493.

[15] Ahedo, E., “ Presheath / sheath, model with Secondary electron emission from two parallel walls,” Physics of Plasma, Vol.), N°10, 2002.

[16] Y.Raitses, D.Staack, M.Keidar, N.J.Fish, “Electron-wall interaction in Hall thrusters” Physics of plasmas, Vol.12, 2005.

[17] G. D. Hobbs and J. A. Wesson. “Heat flow through a Langmir sheath in the presence of electron emission.” Plasma Phys., 9:85, 1967.

[18] L. Jolivet and J.-F. Roussel.” Effects of the secondary electron emission on the sheath phenomenon in a Hall thruster”. In Proc. 3rd International Conference on Spacecraft Propulsion, page 367, Cannes (France), 2000.

[19] A.Dunaevsky, Y.Raitses, N.J.Fisch, “Secondary electron emission from dielectric materials of a Hall thruster with segmented electrodes”, Physics of plasmas, Vol.10, N°6, 2003.

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Modello numerico della scarica in un motore ad effetto Hall

211

[20]Manzella, D., “Predicting Hall Thruster Operational Lifetime”, AIAA 2004- 3953, 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Fort Lauderdale, Florida, July 11-14, 2004.

[21]Peterson, P.Y., and Manzella, D.H., ”Investigation of the Erosion Characteristics of a Laboratory Hall Thruster”, AIAA 2003-5005, 39th

AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Huntsville, AL., July 2003.

[22] Barral, S., “Numerical studies of Hall Thrusters based on fluid equations” ,Tesi di Laurea in ‘Technical Sciences’, Instytut Podstawowych Problemów Techniki Polska Akademia Nauk, 2003.

[23] E. Ahedo and J.M Gallardo, “Scaling down hall thrusters”, IEPC 2003-104.

[24] V. Kim, A. Bishaev, A. Lazourenko, and M. Auwter-Kurtz.” 3-dimensional simulation of plasma dynamics in SPT.”In Proc. 27th International Electric Propulsion Conference, number 01-340, Pasadena, 2001.

[25] M. Hirakawa and Y. Arakawa., “Particle simulation of plasma phenomena in Hall thrusters”. In Proc. 24th International. Electric Propulsion Conference, number 95-164, Moscow, 1995.

[26] M. Hirakawa and Y. Arakawa. “Numerical simulation of plasma particle behavior in a Hall thruster”. In Proc. 32nd AIAA Joint Propulsion Conference, number 96-3195, Lake Buena Vista, 1996.

[27] M. Hirakawa.” Electron transport mechanism in a Hall thruster”. In Proc. 25th International Electric Propulsion Conference, number 97-021, Cleveland, 1997.

[28] J. M. Fife, M. Martinez-Sanchez, and J. Szabo.” A numerical study of low- frequency discharge oscillations in Hall Thrusters”. In Proc. 33rd AIAA Joint Propulsion Conference, number 97-3051, Seattle, 1997.

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Bibliografia

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[29] G. J. M. Hagelaar, J. Bareilles, L. Garrigues, and J.-P. Boeuf. “Parametric study of a stationary plasma thruster using a two-dimensional hybrid model.” In Proc. 27th International Electric Propulsion Conference, number 01-28, Pasadena, 2001.

[30] Szabo., J., J., “Fully kinetic Numerical Modeling of a Plasma Thruster” ,Tesi di Laurea in ‘Aeronautics and Astronautics’, Massachusetts Institute of Technology, 2001.

[31] Manzella, D., H., “Simplified Numerical Description of SPT operation,” NASA Report, IEPC 95-34, 1995.

[32] Ahedo, E.,Gallardo, J. M., Martinez-Sanchez, M. “Model of the plasma discharge in a Hall thruster with heat conduction”, Physics of Plasmas, Vol.9, N°9,2002.

[33] Zwillinger, D., “Handbook of differential equations”, 1991.

[34] Demidovic, B., P., “Fondamenti di calcolo numerico”, 1981.

[35] William H. Press, Brian P. Flannery, Saul A. Teukolsky, William T. Vetterling

“Numerical Recipes, The art of scientific computing, second edition” Cambridge University Press, 1992.

[36] M.Mitchner, C.H. Kruger, “Partially ionized gas”, Stanford, California, 1973.

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