本文就是基于此目的，对不同空气消耗系数下的气体燃料燃烧展开了研究工作。

For this purpose, the gas fuel combustion on different coefficient of air consumption has been described in this dissertation.

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不同膨胀系数时施加脉冲的时刻不变，最优的燃料消耗与膨胀变化量成正比；

Second, the initial point and transfer time are same for different object relative orbit, and the minimum consumption of fuel is proportional to the expansion deflection.

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