发明名称 |
Missile having non-cylindrical propulsion section |
摘要 |
A missile has a non-cylindrical fuselage over at least a portion of its length, with a non-cylindrical propulsion system contained within the non-cylindrical portion of the fuselage. The fuselage and propulsion system are preferably generally elliptical in cross section, with a dimensional ratio of the major axis to the minor axis of from more than 1:1 to about 1.5:1. The missile further includes a guidance system and guidance control features.
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申请公布号 |
US5677508(A) |
申请公布日期 |
1997.10.14 |
申请号 |
US19950515479 |
申请日期 |
1995.08.15 |
申请人 |
HUGHES MISSILE SYSTEMS COMPANY |
发明人 |
FINN, KEVIN P.;SCHWARTZ, II, HOMER H.;CONNEL, TIM S.;SNYDER, RICHARD J.;OH, YOUN H. |
分类号 |
F42B10/42;F42B10/64;F42B15/10;(IPC1-7):F42B15/00 |
主分类号 |
F42B10/42 |
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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