References
- Sengupta A, Fitzgerald D, Owens A. Experimental investigation of discharge plasma magnetic confinement in the NSTAR ion thruster. Pasadena (CA): Jet Propulsion Laboratory, California Institute of Technology; 2005 Jul 10–13.
- Yavuz B, Turkoz E, Celik M. Prototype design and manufacturing method of an 8 cm diameter RF ion thruster. Istanbul: Department of Mechanical Engineering Bogazici University Istanbul; 2013.
- Wang J, Polk J, Brinza D. Ion thruster modeling: particle simulations and experimental validations” Blacksburg (VA); Pasadena (CA): Virginia Polytechnic Institute and State University; USA Jet Propulsion Laboratory; 2003.
- Van Noord JL. Lifetime assessment of the NEXT ion thruster. AIAA 2007-5274; Cleveland (OH): NASA Glenn Research Center; 2007 Jul 8–11.
- Beattie JR. XIPS keeps satellites on track. The Industrial Physicist. 1998 Jun; 4(2):24.
- Beat Tie JR, Williams JD, Robson RR. Flight qualification of an 18-mN xenon ion thruster. IEPC 93-1015, 23rd International Electric Propulsion Conference; Seattle (WA); 1993.
- Patterson MJ, Haag TW, Rawlin VK, et al. NASA 30-cm ion thruster development status. AIAA-1994-2849, 30th Joint Propulsion Conference; Indianapolis (IN); 1994.
- Polk JE, Goebel DM, Katz I, et al. Performance and wear test results for a 20-kW class ion engine with carbon–carbon grids. AIAA-2005-4393, 41st Joint Propulsion Conference; Tucson (AZ); 2005.
- Goebel D, Katz Ira. Fundamentals of electric propulsion: Ion and Hall thrusters. Pasadena (CA): Jet Propulsion Laboratory California Institute of Technology, Wiley; 2008.10.1002/9780470436448
- Killinger R, Bassner H, Leiter H, et al. RITA ion propulsion for artemis. AIAA-2001-3490, 37th Joint Propulsion Conference; Salt Lake City (UT); 2001.
- Ozaki T, Nishida E, Kasai Y, et al. Development status of xenon ion engine subsystem for ETS-VIII. AIAA-2003-2215, 21st International Communications Satellite Systems Conference; Yokohama; 2003.
- Brophy JR, Katz I, Polk JE, et al. Numerical simulations of ion thruster accelerator grid erosion. AIAA-2002-4261; Pasadena (CA): Jet Propulsion Laboratory California Institute of Technology Pasadena, California; 2002.
- Taunay P-YCR, Bilen SG, Micci MM. Numerical simulations of a miniature microwave ion thruster. IEPC-2013-194, Presented at the 33rd International Electric Propulsion Conference; Washington (DC): The George Washington University; 2013.
- OPERA-3D used guide, version 14.0. Cobham technical services, vector field software. Oxford. 2010 Dec.
- Chen FF. Introduction to plasma physics and controlled fusion. 2nd ed., Vol. 1, Plasma Physics. New York and London: Plenum Press; 1974.
- Capacci M, Noci G. Investigation of the RMT thruster plasma parameters and performances. Plasma Devices Oper. 1999;7:33–49. DOI:10.1080/10519999908228757