Evaluation of Plasma Properties in a Microwave Electrothermal Thruster Resonant Cavity by Using Two Fluid Global Model (AIAA 2015-3926)
Joint propulsion conference
01.01.2015
10 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Microwave Electrothermal Thruster Performance
Online Contents | 2007
|Microwave Electrothermal Thruster Power
Online Contents | 1998
|Microwave Electrothermal Thruster Performance
AIAA | 2007
|