NASA NTRS · 19840000019
Improved Spark-Ignitor Circuitry
Abstract
Transformer 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.
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Olschansky, D. G.. 1985-01-01. Improved Spark-Ignitor Circuitry. https://ntrs.nasa.gov/citations/19840000019
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