The result shows the important engine parameters such as thrust and specific impulse I sp change a lot during the fly process.
计算表明空气液化发动机的推力、比冲等重要的总体参数在飞行过程中会有较大的变化。
The characteristics of hybrid engine such as specific impulse, adjustable thrust, safety and low cost were demonstrated.
阐明了固液发动机比冲、可多次启动关机、推力可调、安全性好和成本低等特点。
The analysis showed that there was about 2% specific impulse loss if liquid water was drilled out of engine directly.
分析表明液态水直接排出发动机将导致约2%的比冲损失。
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