首页>
外国专利>
Main-stage solid-propellant rocket motor design
Main-stage solid-propellant rocket motor design
展开▼
机译:主级固体推进火箭发动机设计
展开▼
页面导航
摘要
著录项
相似文献
摘要
A ballistic missile main-stage solid-propellant rocket motor; including a propellant grain configuration tailored to provide required missile ballistic performance, having a center bore, major and minor rear fin slots, and a silver eliminator bore enlargement; utilizing a forward pressure equalizing flap; and designed to accommodate severe operating conditions.
展开▼