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NASA NTRS ยท 19890062312

A premixed hydrogen/oxygen catalytic igniter

Abstract

The catalytic ignition of hydrogen and oxygen propellants was studied using a premixing hydrogen/oxygen injector. The premixed injector was designed to eliminate problems associated with catalytic ignition caused by poor propellant mixing in the catalyst bed. Mixture ratio, mass flow rate, and propellant inlet temperature were varied parametrically in testing, and a pulse mode life test of the igniter was conducted. The results of the tests showed that the premixed injector eliminated flame flashback in the reactor and increased the life of the igniter significantly. The results of the experimental program and a comparison with data collected in a previous program are given.

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BibTeXRIS

Green, James M.. 1989-07-01. A premixed hydrogen/oxygen catalytic igniter. https://ntrs.nasa.gov/citations/19890062312

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