发明名称 Segmented carbon-carbon exit cone assembly
摘要 An exit cone (10) for solid propellant rocket motors or liquid propellant rocket engines is fabri­cated as discrete carbon-carbon segments (12) and subsequently assembled into a cone. Preferably, longitudinal and circumferential supporting stiff­eners (32,34,44) are formed integrally therewith. This segmented construction means that if one part of the cone is flawed or damaged, it is necessary only to replace that part rather than the whole one.
申请公布号 GB2505629(A) 申请公布日期 2014.03.12
申请号 GB19850025645 申请日期 1985.10.17
申请人 MORTON THIOKOL INC 发明人 DONALD C GIEDT;FRANK S INMAN
分类号 F02K1/00;F02K9/97 主分类号 F02K1/00
代理机构 代理人
主权项
地址