FIELD: weaponry, in particular, rocket engineering. SUBSTANCE: body 1 of the guided missile control actuator unit has a wall separating its high-pressure chamber 12 and release chamber 13. Wall 11 has a cavity communicating with the cavities of actuating power cylinder 2 by means of through ducts. Cavity 14 accommodates movable (8) and fixed (9) disks of distributor unit 3. EFFECT: improved design. 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| GUIDED MISSILE CONTROL ACTUATOR UNIT | 1996 |
|
RU2092783C1 |
| GUIDED MISSILE AERODYNAMIC CONTROL ACTUATOR | 1994 |
|
RU2074382C1 |
| GUIDED MISSILE CONTROL ACTUATOR UNIT | 1994 |
|
RU2066834C1 |
| GUIDED MISSILE CONTROL ACTUATOR UNIT | 1995 |
|
RU2089838C1 |
| AIR-DYNAMIC UNIT OF GUIDED MISSILE CONTROL ACTUATOR | 1996 |
|
RU2092782C1 |
| CONTROL ACTIVATOR UNIT OF GUIDED MISSILE | 1998 |
|
RU2149345C1 |
| STEERING DRIVE UNIT OF GUIDED MISSILE | 1997 |
|
RU2121650C1 |
| GUIDED MISSILE CONTROL ACTUATOR UNIT | 1995 |
|
RU2087841C1 |
| GUIDED PROJECTILE | 1998 |
|
RU2150082C1 |
| AIR-DYNAMIC CONTROL ACTUATOR | 2000 |
|
RU2167386C1 |
