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Improved Spark-Ignitor CircuitryTransformer reduces flyback voltage 350 V. Several modifications made to inductive discharge spark-ignitor system for rocket engine, which substantially reduce complexity of circuits and eliminate difficulties associated with component matching.
Document ID
19840000019
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Olschansky, D. G. (Rockwell International Corp.)
Date Acquired
August 12, 2013
Publication Date
January 1, 1985
Publication Information
Publication: NASA Tech Briefs
Volume: 8
Issue: 3
ISSN: 0145-319X
Subject Category
Electronic Components And Circuits
Report/Patent Number
ISSN: 0145-319X
Report Number: MFS-19751
MFS-19751
Accession Number
84B10019
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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