FIELD: missile armament. SUBSTANCE: guided missile, having a canard configuration with a single- channel control system, uses fin cantilevers arranged at an angle of 30 to 40 deg. to the plane of the cantilevers of control surfaces. The cantilevers of control surfaces are installed in the plane passing through the axis of the missile symmetrically between the fin cantilevers. The pads of the fin cantilevers and control surfaces are made in relationship 1: (0.10 to 0.20). EFFECT: enhanced efficiency of missile control, simplified design. 3 dwg
Title | Year | Author | Number |
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RU2358233C1 |
GUIDED MISSILE | 1998 |
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GUIDE PROJECTILE | 1996 |
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GUIDED MISSILE | 2014 |
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GUIDED SHELL | 2013 |
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RU2537357C1 |
CONTROLLED PROJECTILE | 2007 |
|
RU2354922C1 |
GUIDED MISSILE | 2000 |
|
RU2166724C1 |
SPIN-STABILIZED MISSILE | 2003 |
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GUIDED PROJECTILE | 2016 |
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RU2645322C1 |
Authors
Dates
1999-07-20—Published
1998-06-09—Filed