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http://dx.doi.org/10.5139/JKSAS.2008.36.7.703

Mixture Ratio Stabilizer for Liquid Propellant Rocket Engine  

Jung, Tae-Kyu (한국항공우주연구원)
Kwon, Se-Jin (한국과학기술원 항공우주공학과)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.36, no.7, 2008 , pp. 703-711 More about this Journal
Abstract
In this paper, stabilizer which maintains the mixture ratio of gas generator of LRE has been introduced. Design criterion for the ideal performance of stabilizer was derived. Significant parameters on the performance of stabilizer were identified through mathematical model and gas generator system analysis. Also, simulation and test results of the gas generator system showed fair agreement, thus proving the validity of the mathematical model of the stabilizer.
Keywords
Stabilizer; Mixture ratio; Thrust control; LRE;
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