Effect of Propellant Temperature on Efficiency in the Pulsed Plasma Thruster
AFRL MicroPPT Development for Small Spacecraft Propulsion
MicroPPT Development for Small Spacecraft Propulsion
AFRL MicroPPT Development for Small Spacecraft Propulsion
Micropropulsion Research at AFRL (Postprint)
Micropropulsion Research at AFRL
Micropropulsion Options for the TechSat21 Space-Based Radar Flight
Propellant Losses Because of Particulate Emission in a Pulsed Plasma Thruster