发明名称 MISSILE NOSE FAIRING ASSEMBLY
摘要 A separable nose fairing assembly includes a forward, massive portion slidably coupled to a rearward, light portion. Forward sliding movement of the massive portion relative to the light portion is limited by a stop. An explosive actuator is operable to drive the forward portion forwardly until it reaches the stop, whereupon the momentum transferred to the rearward portion is sufficient to pull it off the missile. Due to the high ballistic coefficient of the assembly it follows a ballistic trajectory different from that of the missile, thus minimizing the possibility of damage to the missile.
申请公布号 US5159151(A) 申请公布日期 1992.10.27
申请号 US19870057263 申请日期 1987.04.28
申请人 BRITISH AEROSPACE PUBLIC LIMITED COMPANY 发明人 DRANSFIELD, ALFRED E.;WATERS, PETER G.
分类号 F42B15/36 主分类号 F42B15/36
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