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Liquid Propulsion Systems

With the major target in the research and development of a Liquid Propulsion Systems placed in an upper stage engine and an orbit control engine, we are making efforts in the research and development of engines over an extensive range of thrust from 1 N through 100 kN. Through low toxicity and non-toxic propellants, we are also researching next-generation clean orbit control engines. Further, we are conducting research to develop a propulsion system of high reliability capable of manned flight and interplanetary flight, by observing and analyzing the combustion status of various engines and providing self-contained control in the detection of abnormal states.


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