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Lyon B. King
Ion Space Propulsion Lab Page
"Ions in the Sky" Article
E-mail: lbking@mtu.edu

Office: 1014 MEEM
Phone: 487-2683

 

Associate Professor; PhD, University of Michigan

Space Propulsion, Plasma Physics, Optical Fluid Diagnostics

Research Interests

Dr. King is an experimentalist interested in studying electric space propulsion systems, including Hall-effect thrusters, ion engines, and arcjets. By utilizing strong electromagnetic forces to accelerate an ionized plasma propellant, electric thrusters take advantage of on-orbit solar power generation to enjoy significant fuel savings over traditional chemical rockets. King's research experience in the broader field of plasma physics includes such diverse subjects as the design of the in-situ electrostatic probes, ion-energy analysis and time-of-flight mass spectrometry, Doppler laser cooling of trapped ions, optical flow diagnostics, and antimatter confinement.

Publications

  • King, L. B. and Gallimore, A. D., "Ion Energy Diagnostics in the Plasma Exhaust Plume of a Hall Thruster," Journal of Propulsion and Power, Vol. 16, No. 5, September-October 2000.
  • King, L. B. and Gallimore, A. D., "Identifying Charge-exchange Collision Products within the Ion-energy Distribution of Electrostatically Accelerated Plasmas," Physics of Plasmas, Vol. 6, No. 7, pp. 2936-42, July 1999.
  • King, L. B., Gallimore, A. D., and Marrese, C. M., "Transport-property Measurements in the Plume of an SPT-100 Hall-effect Thruster," Journal of Propulsion and Power, Vol. 14, No. 3, pp. 327-35, May-June 1998.
  • King, L. B. and Gallimore, A. D., "Gridded Retarding Pressure Sensor for Ion and Neutral Particle Analysis in Flowing Plasmas," Review of Scientific Instruments, Vol. 68, No. 2, February 1997.

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