建立了全流量补燃循环发动机的静态特性的数学模型。
The mathematical models of the static characteristics of the full-flow staged combustion cycle rocket engine were presented.
所得的结论对全流量补燃循环发动机气-气喷注器的优化设计有一定的指导意义。
The results presented in this paper may provide valuable reference for the optimization design of the gas-gas injector for full flow staged combustion cycle engine.
以全流量补燃循环氢氧发动机系统为研究对象，对其的动态响应特性进行了研究。
The full flow staged combustion cycle and its superior performance compared to the traditional cycle are discussed.
应用推荐