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 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|