增益矩阵在标准大气条件下设计，并通过相似理论将其扩展到全线。

Gain matrix K is a constant matrix design at sea-level static condition, and should be transformed to actual flight condition with similarity correction factors.

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计算结果表明，高空条件下不同标准大气对远程弹箭射程的影响很大。

The calculation using different atmosphere data shows that the range of long-range shell-rocket is affected obviously by different standard atmospheres.

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在标准大气压和空醚比为3的条件下，由二甲醚部分氧化反应得到的氢气体积分数最大，约为35%；

H2 concentration produces from DME partial oxidation reaction is the largest under atmosphere when air-to-DME ratio is about 3. The maximum is about 35%.

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在标准大气压和空醚比为3的条件下，由二甲醚部分氧化反应得到的氢气体积分数最大，约为35%；

H2 concentration produces from DME partial oxidation reaction is the largest under atmosphere when air-to-DME ratio is about 3. The maximum is about 35%.

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