LOx를 적용한 Lab-Scale 하이브리드 로켓 지상연소시험 설비

Laboratory scale ground firing test facility for hybrid rocket engine using liquid oxygen as oxidizer was constructed. The ground firing test facility is composed of liquid oxygen feeding system, control/data acquisition system and laboratory scale hybrid rocket combustor. The performance data from this cryogenic oxidizer have been obtained where it has been found that some of improvements were necessary to manage the newly constructed firing test facility. Various combustion tests using liquid oxygen are scheduled after the improvements.