发明名称 FRAGMENTING NOZZLE SYSTEM
摘要 A fragmenting nozzle system includes a first nozzle at least partially disposed within a second nozzle. The first nozzle includes an ablative shell, a syntactic foam support disposed between the ablative shell and the second nozzle, and an ignition system disposed at least partially within the syntactic foam support. For example, the ignition system is operable to generate a controlled-energy deflagration pressure wave that fragments the first nozzle but not the second nozzle.
申请公布号 WO2015171411(A1) 申请公布日期 2015.11.12
申请号 WO2015US28423 申请日期 2015.04.30
申请人 AEROJET ROCKETDYNE, INC. 发明人 MCPHERSON, DOUGLASS, SR.
分类号 F02K9/97;F42B15/10 主分类号 F02K9/97
代理机构 代理人
主权项
地址