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Original Articles

Gas Phase Ignition of a Hypergolic Propellant System

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Pages 207-213 | Received 12 Apr 1971, Published online: 10 May 2007
 

Abstract

A method of measuring ignition delay of a gas phase hypergolic propellant system in quasi steady flow and low pressure conditions is described. The effects of ambient pressure, flow parameters and propellant temperature on the gas phase ignition delay of the system nitrogen tetroxide-UDMH are investigated. An empirical equation relating the ignition delay to ambient pressure and temperature is obtained as;

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