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Pulsed Operation of an Ion AcceleratorElectronic circuitry has been devised to enable operation of an ion accelerator in either a continuous mode or a highpeak power, low-average-power pulsed mode. In the original intended application, the ion accelerator would be used as a spacecraft thruster and the pulse mode would serve to generate small increments of impulse for precise control of trajectories and attitude. The present electronic drive circuitry generates the extraction voltage in pulses. Pulse-width modulation can affect rapid, fine control of time-averaged impulse or ion flux down to a minimum level much lower than that achievable in continuous operation.
Document ID
20090008642
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other - NASA Tech Brief
Authors
Wirz, Richard
(California Inst. of Tech. Pasadena, CA, United States)
Gamero-Castano, Manuel
(California Inst. of Tech. Pasadena, CA, United States)
Goebel, Dan
(California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 24, 2013
Publication Date
February 1, 2009
Publication Information
Publication: NASA Tech Briefs, February 2009
Subject Category
Electronics And Electrical Engineering
Report/Patent Number
NPO-44961
Report Number: NPO-44961
Distribution Limits
Public
Copyright
Public Use Permitted.
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