Proceedings of the Korean Society of Propulsion Engineers Conference (한국추진공학회:학술대회논문집)
- Volume y2005m4
- /
- Pages.265-268
- /
- 2005
- /
- 1975-342X(pISSN)
Ignition Experiments of a High Pressure Liquid Propellant Thrust Chamber
실물형 연소기의 점화시험
Abstract
A series of ignition tests had been conducted for a thrust chamber propelled by Jet A-1 and liquid oxygen with a chamber pressure of 52.5 bara and a thrust of 30 tonf. The chamber ignited by a hypergolic fluid, TEAL, keeps its first constant pressure low at
Jet A-1과 액체산소를 추진제로 하는 연소압 52.5 bara 추력 30 tonf급 로켓엔진 연소기의 2단 점화시험을 수행하였다. 점화방식으로 TEAL과 액체산소를 사용한 hypergolic 방식을 사용하였다. 산화제