FIELD: military equipment, missile weaponry. SUBSTANCE: guided missile control actuator unit has a body with end cavities and a piston linked with the controls. Installed in the end cavities of the body are fixed contacts in the form of adjustable screws, and contacts in the form of spring-loaded plates engageable with them are installed on the piston. EFFECT: improved design. 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| STEERING DRIVE UNIT OF GUIDED MISSILE | 1997 |
|
RU2121650C1 |
| GUIDED MISSILE CONTROL ACTUATOR | 1993 |
|
RU2072506C1 |
| GUIDED MISSILE CONTROL ACTUATOR | 1992 |
|
RU2046060C1 |
| CONTROL ACTIVATOR UNIT OF GUIDED MISSILE | 1998 |
|
RU2149345C1 |
| GUIDED MISSILE CONTROL ACTUATOR UNIT | 1994 |
|
RU2066834C1 |
| GUIDED MISSILE CONTROL ACTUATOR UNIT | 1996 |
|
RU2092783C1 |
| AIR-DYNAMIC CONTROL ACTUATOR | 2000 |
|
RU2167386C1 |
| GUIDED MISSILE CONTROL ACTUATOR UNIT | 1995 |
|
RU2087841C1 |
| GUIDED MISSILE CONTROL ACTUATOR UNIT | 1995 |
|
RU2084810C1 |
| GUIDED MISSILE AERODYNAMIC CONTROL ACTUATOR | 1994 |
|
RU2074382C1 |
