Proceedings of the Korean Society of Propulsion Engineers Conference (한국추진공학회:학술대회논문집)
- 2003.10a
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- Pages.131-134
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- 2003
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- 1975-342X(pISSN)
Development of a Hydrogen-Peroxide Rocket Engine of l00N Thrust
l00N $H_2O_2$ Monopropellant 로켓 엔진의 개발
- Sang-Hee Ahn (Kyungpook National University, Graduate School of Mechanical Engineering) ;
- S. Krishnan (Kyungpook National University, School of Mechanical Engineering) ;
- Choog-Won Lee (Kyungpook National University, School of Mechanical Engineering)
- Published : 2003.10.01
Abstract
There has been a renewed interest in the use of hydrogen peroxide as an oxidizer in bipropellant liquid rocket engines as well as in hybrid rocket engines. This is because hydrogen peroxide is a propellant of low toxicity and enhanced versatility. The present paper details the features of the designed engine of l00N thrust and its facility. Also explained is the arrangement of the distillation unit to be used to prepare rocket-grade hydrogen-peroxide propellant. Results of the simulated "cold" tests are presented.