Performance Characteristics of GCH4-LOx Small Rocket Engine According to the Equivalence Ratio Variation at a Constant Pressure of Combustion Chamber (동일한 연소실 압력에서의 당량비 변화에 따른 기체메탄-액체산소 소형로켓엔진의 성능특성)
-
- Journal of the Korean Society of Propulsion Engineers
- /
- v.26 no.6
- /
- pp.34-42
- /
- 2022