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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
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2013
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Article
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Fig 5
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Research Article
Global Modeling of N
2
O Discharges: Helicon Plasma Thruster Application
Figure 5
“Core” region densities of species of a 5 sccm N
2
O fed HPT of 200 W absorbed power. Pressure varies from 5 mTorr to 20 mTorr.