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.
Improved Spark-Ignitor Circuitry
NASA Tech Briefs ; 8 , 3
01.01.1985
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Englisch
FIXING STRUCTURE FOR IGNITOR AND FIXING METHOD FOR IGNITOR
Europäisches Patentamt | 2018
|NTRS | 1994
|Online Contents | 1995