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Electrical performance characteristics of high power converters for space power applicationsThe first goal of this project was to investigate various converters that would be suitable for processing electric power derived from a nuclear reactor. The implementation is indicated of a 20 kHz system that includes a source converter, a ballast converter, and a fixed frequency converter for generating the 20 kHz output. This system can be converted to dc simply by removing the fixed frequency converter. This present study emphasized the design and testing of the source and ballast converters. A push-pull current-fed (PPCF) design was selected for the source converter, and a 2.7 kW version of this was implemented using three 900 watt modules in parallel. The characteristic equation for two converters in parallel was derived, but this analysis did not yield any experimental methods for measuring relative stability. The three source modules were first tested individually and then in parallel as a 2.7 kW system. All tests proved to be satisfactory; the system was stable; efficiency and regulation were acceptable; and the system was fault tolerant. The design of a ballast-load converter, which was operated as a shunt regulator, was investigated. The proposed power circuit is suitable for use with BJTs because proportional base drive is easily implemented. A control circuit which minimizes switching frequency ripple and automatically bypasses a faulty shunt section was developed. A nonlinear state-space-averaged model of the shunt regulator was developed and shown to produce an accurate incremental (small-signal) dynamic model, even though the usual state-space-averaging assumptions were not met. The nonlinear model was also shown to be useful for large-signal dynamic simulation using PSpice.
Document ID
19900004963
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Stuart, Thomas A.
(Toledo Univ. OH, United States)
King, Roger J.
(Toledo Univ. OH, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1989
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NAS 1.26:185947
NASA-CR-185947
Report Number: NAS 1.26:185947
Report Number: NASA-CR-185947
Accession Number
90N14279
Funding Number(s)
CONTRACT_GRANT: NAG3-708
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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