FIELD: transport.
SUBSTANCE: proposed devise is composed of rudder control mechanism and includes two links articulated with aerodynamic and gas rudders. Link coupled with aerodynamic rudder comprises bracket with groove, rocker with opening, link connected with gas rudder and rocker with pin. Rockers are articulated with two tie-rods.
EFFECT: higher reliability of separation.
3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
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|
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| DEVICE OF MISSILE STABILIZATION | 2014 |
|
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|
RU2482434C1 |
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| ROCKET STABILIZATION DEVICE | 2015 |
|
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| DEPLOYABLE RUDDER OF MISSILE | 2013 |
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| METHOD OF MISSILE MOVEMENT STABILIZATION AT UNDERWATER LAUNCH AND DEVICE FOR ITS IMPLEMENTATION | 2015 |
|
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| CONTROLLED BULLET | 2012 |
|
RU2512047C1 |
