Cold Flow Measurements in the Study of Injection Phenomena in Vortex-Type Rocket Engine Injectors.
ROCKET PROPULSION ESTABLISHMENT WESTCOTT (ENGLAND)
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Quantitative studies have been made of the flow of water from an isolated sector of a vortex-type injector. The results are used to explain the phenomena observed on tests made during the development of a packaged propellent rocket engine. A correlation is developed to determine the deflection of the tangentially introduced liquid by a jet injected radially, and this result is shown to be applicable to the design of an injector for the hypergolic propellents mixed amine fuel and inhibited red fuming nitric acid. Author
- Combustion and Ignition
- Liquid Propellant Rocket Engines