The properties of additive methyl silicone and the mechanism of heat flux reduction in the thrust chamber are described.
叙述了添加剂——甲基硅酮的性质和用添加剂降低推力室热流强的机理。
Also the Mohr -coulomb theory of the transfer coefficient reduction method is derived based on thrust calculation and the rigid body limit equilibrium separately.
同时也分别从推力计算和刚体极限平衡条件推导了基于摩尔-库仑理论的传递系数折减法。
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