NASA NTRS · 20120012500
Spark-integrated propellant injector head with flashback barrier
Abstract
High performance propellants flow through specialized mechanical hardware that allows for effective and safe thermal decomposition and/or combustion of the propellants. By integrating a sintered metal component between a propellant feed source and the combustion chamber, an effective and reliable fuel injector head may be implemented. Additionally the fuel injector head design integrates a spark ignition mechanism that withstands extremely hot running conditions without noticeable spark mechanism degradation.
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Mungas, Gregory Stuart, Fisher, David James, Mungas, Christopher. 2012-07-31. Spark-integrated propellant injector head with flashback barrier. https://ntrs.nasa.gov/citations/20120012500
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