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The 30-cm ion thruster power processorA power processor unit for powering and controlling the 30 cm Mercury Electron-Bombardment Ion Thruster was designed, fabricated, and tested. The unit uses a unique and highly efficient transistor bridge inverter power stage in its implementation. The system operated from a 200 to 400 V dc input power bus, provides 12 independently controllable and closely regulated dc power outputs, and has an overall power conditioning capacity of 3.5 kW. Protective circuitry was incorporated as an integral part of the design to assure failure-free operation during transient and steady-state load faults. The implemented unit demonstrated an electrical efficiency between 91.5 and 91.9 at its nominal rated load over the 200 to 400 V dc input bus range.
Document ID
19780016337
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Herron, B. G.
(Hughes Research Labs. Malibu, CA, United States)
Hopper, D. J.
(Hughes Research Labs. Malibu, CA, United States)
Date Acquired
September 3, 2013
Publication Date
April 1, 1978
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-CR-135401
Report Number: NASA-CR-135401
Accession Number
78N24280
Funding Number(s)
CONTRACT_GRANT: NAS3-17223
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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