Computational Investigations of Performance Improvements for Microlaser Ablation Plasma Thrusters Using Nozzles

Recent work has investigated the microlaser ablation plasma thruster, which is a subkilogram form of satellite propulsion. Computational simulations that investigate the microthruster operation by the ablation of plasma through a nozzle using a magnetohydrodynamic code are presented. The performance...

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Bibliographic Details
Published inIEEE transactions on plasma science Vol. 39; no. 11; pp. 2932 - 2933
Main Authors Thompson, R. J., Moeller, T. M.
Format Journal Article
LanguageEnglish
Published New York IEEE 01.11.2011
The Institute of Electrical and Electronics Engineers, Inc. (IEEE)
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