FIELD: armament, in particular, missiles. SUBSTANCE: spaces of actuating power cylinder 12 are formed in the control actuator unit in body 1, they are restricted by back wall 13 with duct 14 connected to the distributing device. The spaces are separated by partition 15 in the form of a semitube. The piston is made in the form of disc plates with cut planes perpendicularly to axis 6 of control fins 5. EFFECT: improved design. 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| STEERING DRIVE UNIT OF GUIDED MISSILE | 1997 |
|
RU2121650C1 |
| CONTROL ACTIVATOR UNIT OF GUIDED MISSILE | 1998 |
|
RU2149345C1 |
| GUIDED MISSILE CONTROL ACTUATOR | 1992 |
|
RU2046060C1 |
| GUIDED MISSILE CONTROL ACTUATOR UNIT | 1995 |
|
RU2089838C1 |
| GUIDED MISSILE CONTROL ACTUATOR | 1993 |
|
RU2072506C1 |
| AIR-DYNAMIC CONTROL ACTUATOR | 2000 |
|
RU2167386C1 |
| GUIDED MISSILE AERODYNAMIC CONTROL ACTUATOR | 1994 |
|
RU2074382C1 |
| GUIDED MISSILE CONTROL ACTUATOR UNIT | 1996 |
|
RU2092783C1 |
| AIR-DYNAMIC UNIT OF GUIDED MISSILE CONTROL ACTUATOR | 1996 |
|
RU2092782C1 |
| AIR-DYNAMIC STEERING DRIVE OF GUIDED MISSILE | 1997 |
|
RU2121651C1 |
