Experimental Investigations of a Krypton Stationary Plasma Thruster

<table>ATON A-3 thrust versus discharge voltage under <svg height="15.1375" id="M37" style="vertical-align:-3.39066pt" version="1.1" viewbox="0 0 59.799999 15.1375" width="59.799999" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink">
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</svg> mg/s and for different Kr anode mass flow rates under <svg height="15.4" id="M38" style="vertical-align:-3.39066pt" version="1.1" viewbox="0 0 64.224998 15.4" width="64.224998" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink">
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</svg> V.</table>

International Journal of Aerospace Engineering

Experimental Investigations of a Krypton Stationary Plasma Thruster

Figure 5