Abstract: Propellant modules for Micro Pulsed Plasma Thrusters, and techniques for bundling propellant modules and for using a two-stage discharge process to increase MicroPPT propellant throughput, and decrease the output voltage required from the power-processing unit are provided.
Type:
Grant
Filed:
July 9, 2002
Date of Patent:
August 3, 2004
Assignee:
W. E. Research LLC
Inventors:
Gregory G. Spanjers, John Schilling, David White