Plasma Reactors and Plasma Thrusters Modeling by Ar Complete Global Models

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<g transform="matrix(.017,-0,0,-.017,.062,11.55)"><path d="M649 676l-22 -187l-33 -2q3 56 -12 94q-8 20 -31.5 26.5t-86.5 6.5h-74l-90 -491q-4 -23 -6 -36.5t1 -25t7 -16.5t18 -9t27 -5t41 -3l-6 -28h-286l4 28q68 5 84 18.5t28 76.5l94 491h-55q-74 0 -100.5 -6t-41.5 -23q-24 -29 -54 -98l-32 1q32 98 53 188h22q7 -18 15 -22
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</svg>, and ionization percentage versus pressure in the core plasma region of a helicon thruster.</table>

International Journal of Aerospace Engineering

fig17

Figure 17

Figure 17: Plasma Reactors and Plasma Thrusters Modeling by Ar Complete Global Models 