FIELD: armament.
SUBSTANCE: the guided artillery projectile has a body with sealing shields, aerodynamic control surfaces formed inside and a base.
An electric igniter and a piston-pusher are installed in the base. Spring-loaded air intakes are formed inside, they are positioned in the grooves of the base and kept in the folded state by the front edge of the control surface. The electric igniter is provided with a chamber, connected to which are gas power cylinders of one way action with a piston-pusher to each control surface. The piston-pusher is made with a guide, groove for installation of the control surface and provided with a stop fastened on the base.
EFFECT: enhanced reliability of guided artillery projectile.
4 cl, 2 dwg
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| GUIDED MISSILE | 2002 |
|
RU2224213C1 |
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RU2237598C2 |
| GUIDED MISSILE CONTROL ACTUATOR UNIT | 1995 |
|
RU2087841C1 |
| METHOD FOR LEAK-PROOFNESS CHECK OF AUTOPILOT UNIT OF GUIDED ARTILLERY PROJECTILES AND DEVICE FOR ITS REALIZATION | 2004 |
|
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| METHOD FOR STRENGTH TEST OF AUTOPILOT UNIT OF GUIDED MISSILE WITH HOMING HEAD AND DEVICE FOR ITS REALIZATION | 2000 |
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RU2173829C1 |
| GUIDED MISSILE CONTROL ACTUATOR UNIT | 1995 |
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RU2084810C1 |
| METHOD AND DEVICE FOR INITIATING AN AIR-DYNAMIC STEERING DRIVE OF A GUIDED AERIAL BOMB, A METHOD FOR CHECKING THE READINESS OF AN AIR-DYNAMIC STEERING DRIVE BEFORE DROPPING A GUIDED AERIAL BOMB, AN AIR-DYNAMIC STEERING GEAR AND CONTROL EQUIPMENT FOR AN AIR-DYNAMIC STEERING DRIVE OF AN AERIAL BOMB | 2020 |
|
RU2748828C1 |
| METHOD OF CHECK-UP OF BRINGING TO SERVICEABLE CONDITION OF SEALED AUTOPILOT UNIT | 1997 |
|
RU2126949C1 |
| GUIDED MISSILE AND METHOD OF ITS ASSEMBLY | 2007 |
|
RU2336490C1 |
| CONTROLLED PROJECTILE, STEERING DRIVE GROUP OF CONTROLLED PROJECTILE, PNEUMATIC DISTRIBUTION DEVICE OF STEERING DRIVE OF CONTROLLED PROJECTILE, MECHANISM OF INITIATION OF STEERING DRIVE OF CONTROLLED PROJECTILE | 2017 |
|
RU2669979C1 |
