发明名称 |
Method and apparatus for stabilizing the in-tube trajectory of a missile |
摘要 |
Apparatus and method for bypassing eject gas around an annular seal disposed between the trailing end of a missile and a launch tube only in an area where the trailing end of the missile is close to the launch tube in order to provide a centering force on the trailing end of the missile to stabilize the in-tube trajectory of the missile during ejection.
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申请公布号 |
US5438905(A) |
申请公布日期 |
1995.08.08 |
申请号 |
US19840622297 |
申请日期 |
1984.06.19 |
申请人 |
WESTINGHOUSE ELECTRIC CORPORATION |
发明人 |
MATHESON, ERIK R.;WADE, JEFFREY S. |
分类号 |
F41F3/073;(IPC1-7):F41F3/04 |
主分类号 |
F41F3/073 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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