Description of methods to increase propellant throughput in a micro pulsed plasma thruster
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United States of America Patent
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Aug 3, 2004
Grant Date -
Feb 20, 2003
app pub date -
Jul 9, 2002
filing date -
Jul 9, 2001
priority date (Note) -
Expired
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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.
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