发明名称 |
MISSILE HAVING NON-CYLINDRICAL PROPULSION SECTION |
摘要 |
A missile (20) has a non-cylindrical fuselage (22b) over at least a portion of its length, with a non-cylindrical propulsion system (34) contained within the non-cylindrical portion (22b) of the fuselage. The fuselage (22b) and propulsion system (34) 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 (20) further includes a guidance system (38) and control features (32).
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申请公布号 |
CA2183279(C) |
申请公布日期 |
1999.12.28 |
申请号 |
CA19962183279 |
申请日期 |
1996.08.14 |
申请人 |
HUGHES MISSILE SYSTEMS COMPANY |
发明人 |
OH, YOUN H.;FINN, KEVIN P.;SCHWARTZ, HOMER H., II;CONNEL, TIM S.;SNYDER, RICHARD J. |
分类号 |
F42B10/42;F42B10/64;F42B15/10;(IPC1-7):F42B15/01 |
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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