Engineering & Technology
Received: 05 Feb 2019 , Published: 07 February 2019
Views: 127 , Download: 50
|1||Ei Ei Khaing|
The world space market evolves towards low-cost solutions, electric propulsion is going to supersede current chemical devices over the next few years. Ion thrusters are the most developed electric engines intended for propelling spacecraft during in space maneuvers, offering the highest efficiencies at reasonable power and thrust levels. Ionic thruster of a satellite provided a changes in velocity, which can be achieved over long periods of time. On the other thruster plays an important role in attitude control operation system (ACS) including station keeping, attitude control, misalignment of satellite position, orbit maneuver and deep space missions.
 D. M. Goebel and I. Katz, “Fundamentals of Electric Propulsion: Ion and Hall Thrusters”, 1st ed. Hoboken, New Jersey: John Wiley & Sons, 2008.
 R. H. Goddard, “The Green Notebooks”, vol. 1, The Dr. Robert H. Goddard Collection at the Clark University Archives, Clark University, Worchester, Massachusetts.
 C. Sánchez, “Design and Performance Analysis Study of an Ion Thruster: Annex,” Terrassa, 2016.
 R. G. Jahn and E. Y. Choueiri, “Electric Propulsion. Technology Programmes,” ESA Publications Division, 2002.
 NASA.gov. (2017). Ion Propulsion: Farther, Faster, Cheaper. Available at:https://www.nasa.gov/centers/glenn/technology/Ion_Propulsion1. html.
 F. F. Chen, “Introduction to Plasma Physics and Controlled Fusion”, vol. 1, New York: Plenum Press, 1984.
 M. Lieberman and A. Lichtenberg, “Principles of Plasma Discharges and Materials Processing”, New York: John Wiley and Sons, 1994.
 R.J. Goldston and P. H. Rutherford, “Introduction to Plasma Physics”, London: Institute of Physics Publishing, 1995..
 D. G. Fearn, Angela S. Cox, D. R. Moffitt, " An investigation of the initiation of hollow cathode discharge " Royal Aircraft Establishment Technical Report.
 Park, Young-Chul, “Hollow Cathode Plasma Source Characteristics”, Lieutenant, Republic of Korea Navy, Korean Naval Academy, 1982.
 G. R. Brewer, “Ion Propulsion Technology and Applications”, New York: Gordon and Breach, 1970.
 J. R. Brophy, I. Katz, J. E. Polk, and J. R. Anderson, “Numerical Simulations of Ion Thruster Accelerator Grid Erosion,”
 I. G. Mikellides, I. Katz, and M. Mandell, “A 1-D Model of the Hall-Effect Thruster with an Exhaust Region,” 37th Joint Propulsion Conference, Salt Lake City, Nevada, July 8–11, 2001.