The mathematical models of the static characteristics of the full-flow staged combustion cycle rocket engine were presented.
建立了全流量补燃循环发动机的静态特性的数学模型。
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.
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 full flow staged combustion cycle and its superior performance compared to the traditional cycle are discussed.
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.
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。
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