액체로켓엔진 연소기의 지상연소시험을 위한 설비 개발

A combustion chamber, one of engine components, must be developed in precedent stage of space launch program. For this, hot-firing tests of combustion chamber are needed. The performance and reliability of the combustion chamber are evaluated in these tests. Construction of the domestic facility for conducting these tests is expected to relieve the problem of depending on the foreign agency. And this facility has an effect on shortening schedule and cost reduction of combustion chamber development. Futhermore, it is considered that the infrastructures of aerospace-related industries are expanded through building up the facility.