Date: 2013-10-22 10:51:46Optical materials Plasma Double layer Langmuir probe Variable Specific Impulse Magnetoplasma Rocket Helicon Electron Helicon Double Layer Thruster Ion thruster Plasma physics Physics Spacecraft propulsion | | Plasma Adiabaticity in a Diverging Magnetic Nozzle IEPC[removed]Presented at the 33rd International Electric Propulsion Conference, The George Washington University, Washington, D.C., USA October 6–10, 2013 J. P. SheeAdd to Reading ListSource URL: www.umich.eduDownload Document from Source Website File Size: 643,16 KBShare Document on Facebook
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