关键词: 液体推进剂火箭发动机;液氧;煤油;燃气发生器;起动试验

Abstract: 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.

Key words: Liquid propellant rocket engine;Liquid oxygen;Kerosene;Gas generator;Starting test