Gas Phase Ignition of a Hypergolic Propellant System
作者： HIROSHI MIYAJIMA , HIROSHI SAKAMOTO
DOI: 10.1080/00102207108952288
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摘要: Abstract A method of measuring ignition delay a gas phase hypergolic propellant system in quasi steady flow and low pressure conditions is described. The effects ambient pressure, parameters temperature on the nitrogen tetroxide-UDMH are investigated. An empirical equation relating to obtained as;
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