推力室比冲
Calculation of the Specific Impulse Loss for Radiative Cooling Thrust Chamber
辐射冷却推力室的比冲损失计算
The effect of operation pressure on the specific impulse of tactical missile solid motors is analyzed from several factors, such as characteristic velocity, thrust coefficient, impulse coefficients of the chamber and nozzle.
从固体发动机的特征速度、推力系数、燃烧室冲量系数和喷管冲量系数等因素出发,分析了发动机工作压强对战术固体火箭发动机比冲的影响。
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