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In this research, we simultaneously conduct optical observation of the combustion dynamics in consecutive pulse firing operations of the MMH/MON3 bipropellant thruster and the measurement of chamber pressure, in order to investigate transient behaviors in the ignition and cutting off phases of pulse firing mode.
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This page is a summary of: Visualization of Pulse Firing Mode in Hypergolic Bipropellant Thruster, Journal of Propulsion and Power, September 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.b37637.
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