FIELD: armament.
SUBSTANCE: the control compartment of a homing artillery projectile has a body with an inner shoulder, homing head, control actuator with folding aerodynamic controls, electric power unit and a control equipment. It comprises a pitch-angle pick-off in the form of an inertial gyro. The control equipment is positioned in the homing head. The body is made in the form of a truncated cone, with the base of the control actuator fastened around the edges of the inner shoulder.
EFFECT: enhanced flying range of the homing artillery projectile.
1 dwg
| Title | Year | Author | Number | 
|---|---|---|---|
| CONTROL COMPARTMENT AND AUTOPILOT UNIT OF HOMING ARTILLERY PROJECTILE | 2004 | 
 | RU2265789C1 | 
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 | RU2339904C2 | 
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 | RU2339905C2 | 
| TWENTY-FOUR-HOUR HIGH-ACCURACY ALL-WEATHER ADJUSTABLE ROLL-STABILIZED AIR BOMBS WITH GLOBAL SATELLITE NAVIGATION UNIT | 2006 | 
 | RU2317515C1 | 
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 | RU2346232C1 | 
| METHOD FOR CONTROL OF SPIN-STABILIZED MISSILE AND GUIDED MISSILE | 2000 | 
 | RU2166727C1 | 
| ROLL-STABILIZED HOMING AERIAL BOMB | 2003 | 
 | RU2247314C1 | 
| 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 | 
| ROLL-STABILIZED AERIAL BOMB | 2003 | 
 | RU2232973C1 | 
| GUIDED MISSILE CONTROL BAY | 2000 | 
 | RU2176377C2 | 
Authors
Dates
2005-12-10—Published
2004-10-21—Filed