Title: Experimental investigation for hydrogen/oxygen engine using gas dynamic resonance ignition technique
Abstract: Gas dynamic resonance ignition technique was used in design of hydrogen/oxygen small thrust rocket engine. By means of analysis of special impulse and combustion gas temperature in different mixture rate,system parameters of hydrogen/oxygen small thrust rocket engine were determined. Ignition tests of gas dynamic resonance igniter,hot firing tests of hydrogen/oxygen small thrust rocket engine and impulse ignition tests were carried out in different thrust operation conditions. It can be confirmed from the hot firing tests that hydrogen/oxygen small thrust rocket engine can realized multi-restart and stable performance. This may verify the reliability and feasibility of the hydrogen/oxygen small thrust rocket engine.
Publication Year: 2010
Publication Date: 2010-01-01
Language: en
Type: article
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