有没有通用的动力学、热化学理论可用，可完全替代传统的纯理论计算模型实验的实验室工作。
There is no universal kinetic or thermochemical theory available, which could entirely substitute traditional experimental laboratory work with pure theoretical calculation models.
该文提出描述液体工质电热化学发射装置中燃烧过程的理论模型。
A theoretical model has been presented to describe the combustion process in a liquid propellant electrothermal chemical launcher.
液相采用UNIQUAC模型，汽相采用“化学理论”，用回归所得的参数进行汽—液平衡数据的推算，获得了较好的结果。
UNIQUAC model was used for liquid phase and "chemical theory" for vapor phase. The regressing parameters were used to estimate vapor-liquid equilibrium data, and good results were obtained.
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