FIELD: armament, in particular - military equipment.
SUBSTANCE: an air bleeder and escape canals are made in the guided missile. A foundation with power cylinders coupled with the control surfaces, control electromagnet and a distribution device is installed in the control actuator unit. The area of the air bleeder in relation with the area of the escape canals makes up (0.15-0.25):1. The foundation separates the cavity of the control actuator unit into the high-pressure cavity and the escape cavity. The high-pressure cavity is made in relation (5-9) of the volumes of the working cavities of the power cylinders, and the area of the air bleeder is made in relation (5-9) of the areas of the channels of the distribution device.
EFFECT: simplified structure, reduced overall dimensions, weight and cost of the missile.
2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| GUIDED MISSILE | 2005 |
|
RU2295698C1 |
| GUIDED MISSILE AERODYNAMIC CONTROL ACTUATOR | 1994 |
|
RU2074382C1 |
| GUIDED PROJECTILE | 1998 |
|
RU2150082C1 |
| AIR-DYNAMIC CONTROL ACTUATOR | 2000 |
|
RU2167386C1 |
| GUIDED MISSILE NOSE CONE | 1995 |
|
RU2089834C1 |
| STEERING DRIVE UNIT OF GUIDED MISSILE | 1997 |
|
RU2121650C1 |
| GUIDED MISSILE ACTUATOR ASSEMBLY | 1996 |
|
RU2101665C1 |
| TWO-CHANNEL AIR-DYNAMIC UNIT OF GUIDED MISSILE CONTROL ACTUATOR | 2002 |
|
RU2224214C2 |
| GUIDED MISSILE CONTROL ACTUATOR UNIT | 1997 |
|
RU2124697C1 |
| 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 |
