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 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。
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