Global Modeling of N<sub>2</sub>O Discharges: Helicon Plasma Thruster Application

<table>Comparison of the variations of  <svg height="15.8375" id="M90" style="vertical-align:-3.3907pt" version="1.1" viewbox="0 0 17 15.8375" width="17" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink">
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</svg>, ionization percentage for the “core” region of a N<sub>2</sub>O fed, and of an air fed HPT, as a function of absorbed power for 7 mTorr.</table>

International Journal of Aerospace Engineering

fig17

Figure 17

Figure 17: Global Modeling of N<sub>2</sub>O Discharges: Helicon Plasma Thruster Application 

International Journal of Aerospace Engineering

Global Modeling of N2O Discharges: Helicon Plasma Thruster Application

Figure 17

Global Modeling of N₂O Discharges: Helicon Plasma Thruster Application