Plasma properties in the 15-cm-diameter thruster-flowrate.4.7 g/h; propellant utilization efficiency.77% . . . . . . . . . . . . . . . 3 .Plasma properties in the 15-cm-diameter thruster-flowrate, 4.7 g/h; propellant utilization efficiency
No takes yet. Share an insight, caveat, or question.
T. D. Masek (1971) studied this question.
Synapse has enriched 5 closely related papers on similar clinical questions. Consider them for comparative context: