摘要
针对反推发动机由倾斜安装方式更改为垂直安装方式的布局形式变化,进行了初步的理论分析,而后通过编程计算,详细分析了两种布局形式下返回舱着陆速度、着陆姿态的变化情况,计算结果可为发动机的布局设计提供一定参考。
The layout obliquity of retro-rocket was changed from fastigiated installation to vertical installation.Aiming at the change of retrorocket layout,theoretics analysis was carried through primarily in the paper at first,then though program calculation,the landing velocity and landing attitude of return capsule under two different layouts were analysed in detail,and the calculation result can provide certain reference for design of retro-rocket layout.
出处
《航天返回与遥感》
2010年第2期1-9,共9页
Spacecraft Recovery & Remote Sensing
关键词
反推发动机
布局
返回舱
着陆姿态
飞船
Retro-rocket Layout Return capsule Landing attitude Spacecraft
