FIELD: rocket engineering. SUBSTANCE: steering drive unit of guided missile is manufactured in the form of body, power cylinder with piston and steering machine with switch gear. Body has rests limiting turns of piston to both sides through angle with which space of part of cylinder behind piston is related to area of inlet to space of cylinder and to area of switch gear as 1.0:(0.02-0.1):(0.06-0.3). EFFECT: enhanced dynamic characteristics of steering drive unit. 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| CONTROL ACTIVATOR UNIT OF GUIDED MISSILE | 1998 |
|
RU2149345C1 |
| GUIDED MISSILE CONTROL ACTUATOR | 1993 |
|
RU2072506C1 |
| GUIDED MISSILE CONTROL ACTUATOR UNIT | 1997 |
|
RU2138764C1 |
| GUIDED MISSILE AERODYNAMIC CONTROL ACTUATOR | 1994 |
|
RU2074382C1 |
| GUIDED MISSILE CONTROL ACTUATOR UNIT | 1994 |
|
RU2066834C1 |
| AIR-DYNAMIC UNIT OF GUIDED MISSILE CONTROL ACTUATOR | 1996 |
|
RU2092782C1 |
| GUIDED MISSILE CONTROL ACTUATOR UNIT | 1996 |
|
RU2092783C1 |
| GUIDED MISSILE CONTROL ACTUATOR UNIT | 1995 |
|
RU2089838C1 |
| AIR-DYNAMIC STEERING DRIVE OF GUIDED MISSILE | 1997 |
|
RU2121651C1 |
| GUIDED PROJECTILE | 1998 |
|
RU2150082C1 |
