摘要
介绍了液氧／煤油为工质的燃气发生器试验研究方法和结果，着重讨论了发生器在低混合比条件下点火、起动方案和性能参数。
A method and test results of a LOX/kerosene gas generator are described emphatically on the scheme of ignition, starting and performance under low mixture ratio conditions. The experimental investigation was conducted to grasp technique of ignition and starting and to obtain data of performance.It provides basis for demonstration of a new type of engine.
出处
《推进技术》
EI
CAS
CSCD
北大核心
1994年第4期58-61,共4页
Journal of Propulsion Technology
关键词
液体推进剂
火箭发动机
液氧
煤油
Liquid propellant rocket engine, Liquid oxygen, Kerosene, Gas generator, Starting test
