首页>
外国专利>
Adaptable solid-hybrid rocket for crew escape and orbital injection propulsion
Adaptable solid-hybrid rocket for crew escape and orbital injection propulsion
展开▼
机译:适应性强的混合动力火箭,用于机组人员逃生和轨道注入推进
展开▼
页面导航
摘要
著录项
相似文献
摘要
The present invention relates to a propulsion system for transporting a crew transfer vehicle. The propulsion system has a casing which defines a chamber, a solid propellant system positioned within the chamber for generating one of emergency escape propulsion during an emergency portion of an ascent flight and orbital injection propulsion during normal flight operations, and a sustain propulsion system communicating with the chamber for sustaining one of the emergency escape propulsion during the emergency portion of the ascent flight and orbital injection propulsion during the normal flight operations. In one embodiment of the present invention, the sustain propulsion system comprises a hybrid solid fuel grain and liquid oxidizer system. In a second embodiment of the present invention, the secondary propulsion system comprises a liquid fuel and liquid oxidizer system.
展开▼