FIELD: weaponry.
SUBSTANCE: invention relates to arms. The proposed shell comprises a homing head, nose unit with its casing fixed on the said homing head and housing a piston with pyrotechnical device and spring. The said piston can move towards the joint with the head and rests upon the head bearing surface.
EFFECT: higher reliability of homing shell.
1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| NOSE UNIT OF HOMING PROJECTILE | 2004 |
|
RU2266512C1 |
| METHOD FOR SEPARATION OF GUIDED MISSILE NOSE BLOCK WITH HOMING HEAD AND DEVICE FOR ITS REALIZATION | 2002 |
|
RU2212628C1 |
| METHOD FOR INCREASING THE FLYING RANGE OF HOMING PROJECTILE AND HOMING PROJECTILE | 2004 |
|
RU2265788C1 |
| ARTILLERY GUIDED MISSILE | 2002 |
|
RU2214580C1 |
| ARTILLERY GUIDED PROJECTILE | 2002 |
|
RU2205357C1 |
| CONTROL COMPARTMENT AND AUTOPILOT UNIT OF HOMING ARTILLERY PROJECTILE | 2004 |
|
RU2265789C1 |
| HOMING PROJECTILE | 2023 |
|
RU2816161C1 |
| BALLISTIC CAP OF ARTILLERY GUIDED MISSILE | 1995 |
|
RU2089837C1 |
| METHOD FOR STRENGTH TEST OF AUTOPILOT UNIT OF GUIDED MISSILE WITH HOMING HEAD AND DEVICE FOR ITS REALIZATION | 2000 |
|
RU2173829C1 |
| DETACHABLE NOSE CONE OF GUIDED MISSILE | 1997 |
|
RU2124175C1 |
