FIELD: armament.
SUBSTANCE: the guided missile has a body with a warhead fastened to its front end, control equipment module fastened in the rear end of the missile body, and an electric wire bundle with a compensator of longitudinal motions. The warhead has a telescope joint to the control equipment module by means of a cylindrical bush that is fastened to the control equipment module by radial pins. The bush and the warhead are fixed to each other by a cut component, whose breaking force is less than the cutting force of the pins. The length of the telescope fit of the cylindrical bush exceeds the linear elongation of the missile body at a kinetic heating.
EFFECT: enhanced maneuverability of the missile.
2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| GUIDED MISSILE | 2003 |
|
RU2239781C1 |
| GUIDED PROJECTILE | 2005 |
|
RU2288438C1 |
| GUIDED MISSILE | 2004 |
|
RU2244896C1 |
| GUIDED PROJECTILE | 2008 |
|
RU2380649C1 |
| CONTROL UNIT OF GUIDED SPIN-STABILIZED MISSILE | 2005 |
|
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| CONTROLLED PROJECTILE | 2010 |
|
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| UNIVERSAL ARTILLERY COMPLEX FOR TELESCOPIC CARTRIDGE | 2018 |
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|
RU2538881C1 |
| UNIT OF THE CONTROL SYSTEM OF A ROCKET LAUNCHED FROM A TUBULAR GUIDE | 2022 |
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RU2799899C1 |
