发明名称 Gas strut separation for staged rocket
摘要 A staged rocket apparatus includes first and second stages connected by a releasable connector. A plurality of pressurized gas struts are connected between the first and second stages and provide a separating force urging the first and second stages apart. The gas struts are held in a telescopingly collapsed first position by the releasable connector. The separating force is maintained at a minimum value so long as the releasable connector holds the struts in their first position. When the releasable connector is disconnected the separating force increases due to gas flow through a metering passage having a progressively increasing flow area from a high pressure chamber to a low pressure chamber.
申请公布号 US8091481(B1) 申请公布日期 2012.01.10
申请号 US20090434388 申请日期 2009.05.01
申请人 FLOYD BRIAN A. 发明人 FLOYD BRIAN A.
分类号 F42B15/10 主分类号 F42B15/10
代理机构 代理人
主权项
地址