Comprehensive design method for lox/liquid-methane regenerative cooling combustor with coaxial injector

被引：0
|
作者：
Yatsuyanagi, Nobuyuki [1 ]
机构：
[1] Kakuda Research Center, National Aerospace Laboratory, Formerly, Kakuda, Japan
来源：
Transactions of the Japan Society for Aeronautical and Space Sciences | 2009年 / 52卷 / 177期
关键词：
Rocket engines;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
Journal article (JA)
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收藏
页码：180 / 187
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