发明名称 |
GUIDED MISSILE |
摘要 |
armament, applicable in small-sized rockets and artillery projectiles. SUBSTANCE: guided missile has a body with a warhead and a control equipment located behind it. The external surface of the body in the area positioned in the junction of the warhead and the front part of the equipment is provided with longitudinal bulges, and a cavity communicating with the missile rear end is formed between the inner surface of the body and the control equipment. EFFECT: reduced kinetic heating of the body and control equipment due to reduced heat transfer from the boundary layer of the incoming air layer to the body and control equipment. 1 dwg
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申请公布号 |
RU2176069(C2) |
申请公布日期 |
2001.11.20 |
申请号 |
RU20000101458 |
申请日期 |
2000.01.17 |
申请人 |
GOSUDARSTVENNOE UNITARNOE PREDPRIJATIE "KONSTRUKTO;GUP KONSTRUKTO |
发明人 |
ZHUKOV V.P.;BIRJUKOV D.L.;KUZNETSOV V.M. |
分类号 |
F42B15/34;F42B15/00;(IPC1-7):F42B15/34 |
主分类号 |
F42B15/34 |
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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