The results present thrust, specificimpulse 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。
2
As the length of secondary combustion chamber increases, the thrust, specificimpulse and combustion efficiency increase respectively.