FIELD: armament.
SUBSTANCE: the control actuator pod of the guided projectile has a base with power cylinders, control electromagnet and a distribution device installed on it. Ducts are made in the projectile longitudinal axis, the cylindrical sections of the power cylinder bodies with inlets, a duct for installation of the distribution device pick-up are located in these ducts. Ducts connecting the pick-up cavities to the power cylinder cavities are made in the plane perpendicular to the projectile axis.
EFFECT: simplified construction of the projectile, enhanced its reliability, reduced weight and cost of the projectile.
3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| TWO-CHANNEL AIR-DYNAMIC UNIT OF GUIDED MISSILE CONTROL ACTUATOR | 2002 |
|
RU2224214C2 |
| CONTROL ACTUATOR UNIT OF GUIDED MISSILE | 2004 |
|
RU2276771C2 |
| GUIDED MISSILE | 2005 |
|
RU2295698C1 |
| 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 |
| GUIDED MISSILE AERODYNAMIC CONTROL ACTUATOR | 1994 |
|
RU2074382C1 |
| GUIDED MISSILE CONTROL ACTUATOR UNIT | 1994 |
|
RU2066834C1 |
| GUIDED MISSILE CONTROL ACTUATOR | 1993 |
|
RU2072506C1 |
| CONTROL ACTUATOR OF GUIDED MISSILE | 2004 |
|
RU2257534C1 |
| ACTUATOR OF GUIDED PROJECTILE | 2004 |
|
RU2282134C2 |
| AIR-DYNAMIC STEERING DRIVE OF GUIDED MISSILE | 1997 |
|
RU2121651C1 |
