NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Advances in solid state switchgear technology for large space power systemsHigh voltage solid state remote power controllers (RPC's) and the required semiconductor power switches to provide baseline technology for large, high power distribution systems in the space station, all electric airplane and other advanced aerospace applications were developed. The RPC's were developed for dc voltages from 28 to 1200 V and ac voltages of 115, 230, and 440 V at frequencies of 400 Hz to 20 kHz. The benefits and operation of solid state RPC's and highlights of several developments to bring the RPC to technology readiness for future aerospace needs are examined. The 28 V dc Space Shuttle units, three RPC types at 120 V dc, two at 270/300 V dc, two at 230 V ac and several high power RPC models at voltages up to 1200 V dc with current ratings up to 100 A are reviewed. New technology programs to develop a new family of (DI)2 semiconductor switches and 20 kHz, 440 V ac RPC's are described.
Document ID
19840014823
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sundberg, G. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1984
Subject Category
Electronics And Electrical Engineering
Report/Patent Number
E-2096
NAS 1.15:83652
NASA-TM-83652
Report Number: E-2096
Report Number: NAS 1.15:83652
Report Number: NASA-TM-83652
Meeting Information
Meeting: Intersoc. Energy Conversion Eng. Conf.
Location: San Francisco, CA
Country: United States
Start Date: August 19, 1984
End Date: August 24, 1984
Accession Number
84N22891
Funding Number(s)
PROJECT: RTOP 506-55-72
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available