The results present thrust, specific impulse and thrust efficiency of the thruster under various environmental pressures, as well as impulse density distribution on the exit plane.
计算结果给出了不同环境压强下推力器的推力、比冲、推进效率和出口平面冲量密度分布。
As the length of secondary combustion chamber increases, the thrust, specific impulse and combustion efficiency increase respectively.
随着补燃室长度的增大，发动机推力、比冲和燃烧效率均提高。
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