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

<table> “Core” region densities of species of a N<sub>2</sub>O fed HPT of 50 W absorbed power. Pressure varies from 3 mTorr to 10 mTorr.</table>

International Journal of Aerospace Engineering

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