液体火箭发动机由摇摆喷管、燃料混合室、燃烧室、涡轮泵、燃烧剂泵、氧化剂泵、燃料输送管路、火药启动装置及各种活门等复杂系统构成。燃烧剂和氧化剂分别贮存在两个隔离的贮箱内,通过管路和加压泵挤压到发动机燃烧室进行混合自行点燃,从喷管排出产生推力。
液体推进剂的晃动特性对大型液体运载火箭以及战略弹道导弹的飞行动力稳定性有着很大的影响。
The dynamic behavior of the liquid sloshing has great effect on the dynamic stability of the liquid filled space vehicle and the strategical ballistic missile.
它正在逐步地采用固体燃料导弹更换它陈旧的、液体燃料核弹道导弹,将使这些导弹发射更快和更为灵活。
It is gradually replacing its older, liquid-fueled ballistic nuclear-capable missiles with solid-fuel missiles, which will make launching them faster and less cumbersome.
液体推进剂的晃动特性对大型液体运载火箭以及战略弹道导弹的飞行动力稳定性有着很大的影响。
The dynamic behavior of the liquid sloshing has great effect on the dynamic stability of the liquid filled space vehicle and the strategical ballistic missle.
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