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Simplified power supplies for ion thrustersThe initial development and demonstration of power supplies with an order of magnitude reduction in parts count, leading to increased reliability at lower weight, while still maintaining thrust system performance are discussed. Two new self-regulating keeper power supply circuits were developed and tested. One supply comprises 14 parts and uses an input voltage range of 18 to 36 volts, the other operates from 200 to 400 volts and requires 22 components. A technique for controlling heater power is also demonstrated.
Document ID
19810011649
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Gruber, R. P.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1981
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
E-765
NASA-TM-81725
Report Number: E-765
Report Number: NASA-TM-81725
Meeting Information
Meeting: Intern. Elec. Propulsion Conf.
Location: Las Vegas, NV
Country: United States
Start Date: April 21, 1981
End Date: April 23, 1981
Accession Number
81N20177
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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