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Solid state power controllersThe rationale, analysis, design, breadboarding and testing of the incremental functional requirements are reported that led to the development of prototype 1 and 5 Amp dc and 1 Amp ac solid state power controllers (SSPC's). The SSPC's are to be considered for use as a replacement of electro-mechanical relays and circuit breakers in future spacecraft and aircraft. They satisfy the combined function of both the relay and circuit breaker and can be remotely controlled by small signals, typically 10 mA, 5 to 28 Vdc. They have the advantage over conventional relay/circuit breaker systems in that they can be located near utilization equipment and the primary ac or dc bus. The low level control, trip indication and status signals can be circuited by small guage wire for control, computer interface, logic, electrical multiplexing, unboard testing, and power management and distribution purposes. This results in increased system versatility at appreciable weight saving and increased reliability.
Document ID
19740004322
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Gibbs, R. S.
(Teledyne Systems Corp. Hawthorne, CA, United States)
Date Acquired
September 3, 2013
Publication Date
August 30, 1973
Subject Category
Physics, Solid-State
Report/Patent Number
NASA-CR-134134
Report Number: NASA-CR-134134
Accession Number
74N12435
Funding Number(s)
CONTRACT_GRANT: NAS9-12914
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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