Physics
Scientist
Application of Pulsed Plasma Thrusters for Small Satellites
APPT for LEO Applications
Comparative Analysis of PPT amd SPT Propulsion Systems for a Given Thrust Total Impulse
Correction Propulsion System with Ablative Pulsed Plasma Thrusters for Unified Space Platform 'Vulcan'
Dynamics of Electric Fields in the Near-Surface Region of Spacecraft during Plasma Ejection from the Mir Orbital Station
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