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Resonant AC power system proof-of-concept test programProof-of-concept testing was performed on a 20-kHz, resonant power system breadboard from 1981 through 1985. The testing began with the evaluation of a single, 1.0-kW resonant inverter and progressed to the testing of breadboard systems with higher power levels and more capability. The final breadboard configuration tested was a 25.0-kW breadboard with six inverters providing power to three user-interface modules over a 50-meter, 20-kHz bus. The breadboard demonstrated the ability to synchronize multiple resonant inverters to power a common bus. Single-phase and three-phase 20-kHz power distribution was demonstrated. Simple conversion of 20-kHz to dc and variable-frequency ac was demonstrated as was bidirectional power flow between 20-kHz and dc. Steady state measurements of efficiency, power-factor tolerance, and conducted emissions and conducted susceptibility were made. In addition, transient responses were recorded for such conditions as start up, shut down, load changes. The results showed the 20-kHz resonant system to be a desirable technology for a spacecraft power management and distribution system with multiple users and a utility-type bus.
Document ID
19870020305
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Wappes, Loran J.
(General Dynamics Corp. San Diego, CA, United States)
Date Acquired
September 5, 2013
Publication Date
October 1, 1986
Subject Category
Electronics And Electrical Engineering
Report/Patent Number
NASA-CR-175069-VOL-1
NAS 1.26:175069-VOL-1
Report Number: NASA-CR-175069-VOL-1
Report Number: NAS 1.26:175069-VOL-1
Accession Number
87N29738
Funding Number(s)
CONTRACT_GRANT: NAS3-22777
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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