NASA NTRS · 19680000338
Two-fluid, impinging-sheet injector
Abstract
Two-fluid, impinging-sheet propellant injector reduces the severe erosion found to occur when ejector elements are directly exposed during throttling without the benefits of a cooling flow of the propellant liquids. It greatly improves combustion efficiency by venting the secondary stream of combustion gases generated by backspray reaction.
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Riebling, R. W.. 1968-09-01. Two-fluid, impinging-sheet injector. https://ntrs.nasa.gov/citations/19680000338
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