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The Calculated Performance of Ethyl Alcohol-Water Mixtures as Rocket Fuels with Liquid Oxygen

机译：液 - 氧火箭燃料乙醇 - 水混合物的计算性能

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Specific impulses and combustion temperatures have been calculated for rocket propellants consisting of liquid oxygen and ethyl alcohol-water mixtures. This system appears to have a number of advantages compared with the corresponding liquid oxygen and petrol system.

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A. B. P. BEETON;
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年度 1953
页码 1-10
总页数 10
原文格式 PDF
正文语种 eng
中图分类工业技术;
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The Calculated Performance of Ethyl Alcohol-Water Mixtures as Rocket Fuels with Liquid Oxygen

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