Design of a three-phase, 15-kilovolt-ampere static inverter for motor-starting a Brayton space power system

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086 0 ‡aNAS 1.14:D-6602
088 ‡aNASA-TN-D-6602
100 1 ‡aFrye, Robert J.
245 1 0 ‡aDesign of a three-phase, 15-kilovolt-ampere static inverter for motor-starting a Brayton space power system / ‡cRobert J. Frye and Arthur G. Birchenough.
246 3 ‡aNASA TN D-6602
246 3 ‡aDesign of a 3-phase, 15-kilovolt-ampere static inverter for motor-starting a Brayton space power system
260 ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration : ‡b[For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], ‡c1972.
300 ‡a20 p. : ‡bill. ; ‡c27 cm.
490 0 ‡aNASA technical note ; ‡vD-6602
504 ‡aIncludes bibliographical references (p. 20).
520 ‡aThe design of a three-phase, 400-Hz, 15-kVA static inverter for motor-starting the 2- to 15-kWe Brayton electrical space power system is described. The inverter operates from a nominal 56-V dc source to provide a 28-V, rms, quasi-square-wave output. The inverter is capable of supplying a 200-A peak current. Integrated circuitry is used to generate the three-phase, 400-Hz reference signals. Performance data for a drive stage that improves switching speed and provides efficient operation over a range of output current and drive supply voltage are presented. A transformerless, transistor output stage is used.
538 ‡aMode of access: Internet.
650 0 ‡aSpace vehicles ‡xAuxiliary power supply ‡xBrayton cycle.
650 0 ‡aBrayton cycle.
650 0 ‡aElectric inverters.
700 1 ‡aBirchenough, Arthur G.
710 2 ‡aLewis Research Center.
710 1 ‡aUnited States. ‡bNational Aeronautics and Space Administration.
CID ‡a011444985
DAT 0 ‡a20101110151310.0 ‡b20141009010000.0
DAT 1 ‡a20141112165512.0 ‡b2023-03-14T18:36:06Z
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