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scientific edition of Bauman MSTUSCIENCE & EDUCATIONBauman Moscow State Technical University. El № FS 77 - 48211. ISSN 1994-0408
The influence of the azimuthal deviation ion plasma jet on the traction motor efficiency with anode layer
# 12, December 2012 DOI: 10.7463/1212.0483944
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References 1. Gorshkov O.A., Muravlev V.A., Shagaida A.A. Khollovskie i ionnye plazmennye dvigateli dlia kosmicheskikh apparatov [Hall and ion plasma engines for spacecrafts]. Moscow, Mashinostroenie, 2008. 280 p. 2. Grishin S.D., Leskov L.V. Elektricheskie raketnye dvigateli [Electric rocket engines]. Moscow, Mashinostroenie, 1989. 216 p. 3. Grishin S.D. Osnovy teorii elektricheskikh raketnykh dvigatelei. Ch. 1. Vvedenie. Elektrostaticheskie dvigateli [Fundamentals of the theory of electric rocket engines. Pt 1. Introduction. Electrostatic engines]. Moscow, Mashinostroenie, 1999. 119 p. 4. Domonkos M.T., Patterson M.J., Jankovsky R.S. Ion Engine and Hall Thruster development at the NASA Glenn Research Center. International Mechanical Engineering Congress, New Orleans, LA, USA, 17-22 November 2002, 2002, IMECE 2002-34444. 5. Manzella D., Jankovsky R., Hofer R. Laboratory Model 50-kW Hall Thruster. AIAA Papers (Conference Proceedings). 2002. AIAA-2002-3676. 6. Kieckhafer A.W., King L.B. Energetics of Propellant Options for High-Power Hall Thrusters. Journal of Propulsion and Power, January-February 2007, vol. 23, no. 1, pp. 21-26. DOI: 10.2514/1.16376 7. Garrigues L. Study of a Hall effect thruster working with ambient atmospheric gas as propellant for low orbit missions. 32nd International Electric Propulsion Conference, Wiesbaden, Germany, Sept. 11-15, 2011, IEPC-2011-142. 8. Sengupta A., Cappelli M., Tverdokhlebov S. An Overview of the VHITAL Program: A Two-Stage Bismuth Fed Very High Specific Impulse Thruster with anode layer. 29th International Electric Propulsion Conference, 2005, IEPC-2005-238. 9. Babichev A.P., Babushkina N.A., Bratkovskii A.M., et al. Fizicheskie velichiny: Spravochnik [Physical quantities: Handbook]. Moscow, Energoatomizdat, 1991. 1232 p. 10. Emsley J. The Elements. 2nd ed. Clarendon Press, Oxford, 1991. 251 p. (Russ. ed.: Emsli Dzh. Elementy. Moscow, Mir, 1993. 256 p.). 11. Vorob'ev E.V., Dukhopel'nikov D.V., Ivakhnenko S.G., Marakhtanov M.K. Poteria tiagi v dvigateliakh s anodnym sloem za schet azimutal'noi zakrutki ionov [Loss of traction in the engines with anode layer due to azimuthal swirl of ions]. Vestnik MGTU im. N.E. Baumana. Ser. Mashinostroenie [Herald of the Bauman MSTU. Ser. Mechanical Engineering], 2011, spec. iss. “Ionno-plazmennye tekhnologii” [“Ion-plasma technology”], pp. 58-63. 12. Vorob'ev E.V., Dukhopel'nikov D.V., Ivakhnenko S.G., Zhukov A.V., Kirillov D.V., Marakhtanov M.K. Khollovskii uskoritel' s fokusirovannym puchkom dlia nanorazmernoi obrabotki krupnogabaritnykh zerkal opticheskikh teleskopov [Hall accelerator with a focused beam for nanoscale processing of large-sized mirrors of optical telescopes]. Vestnik MGTU im. N.E. Baumana. Ser. Mashinostroenie [Herald of the Bauman MSTU. Ser. Mechanical Engineering], 2011, spec. iss. “Ionno-plazmennye tekhnologii” [“Ion-plasma technology”], pp. 35-41. 13. Massey D.R. Development of a direct evaporation bismuth Hall thruster. Ph.D. Dissertation, University of Michigan, 2008. Publications with keywords: anode layer thruster, anode efficiency, the plasma flow, the azimuthal deflection of ions Publications with words: anode layer thruster, anode efficiency, the plasma flow, the azimuthal deflection of ions See also: Thematic rubrics: Поделиться:
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