FIELD: armament.
SUBSTANCE: the folding aerodynamic control of a guided missile has blades and cylindrical springs installed on both sides of a journal on supporting pins perpendicularly to the axis of blade folding. The journal surface is made in the form of a cam provided with a shoulder coinciding with the slot of the blade in its unfolded position. The blades are provided with a pusher with an impulse powder charge. The cam surface is cylindrical with a variable radius relative to the lade folding axis, and on the side of the shoulder it is plane, perpendicular to the journal axis. The shoulder is inclined relative to the plane passing through the folding axis perpendicularly to the missile axial line, and the shoulder face nearest to the cam is made with a chamfer.
EFFECT: enhanced precision and reliability of operation of the aerodynamic control of the guided missile.
4 cl, 6 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| COLLAPSIBLE AERODYNAMIC MEMBER | 2001 |
|
RU2197704C1 |
| FOLDING AERODYNAMIC MEMBER OF GUIDED PROJECTILE | 2004 |
|
RU2280230C1 |
| FORLING AERODYNAMIC UNIT | 2003 |
|
RU2243488C1 |
| METHOD FOR CONTROL OF SPIN-STABILIZED MISSILE AND GUIDED MISSILE | 2004 |
|
RU2275584C2 |
| GUIDED PROJECTILE | 2001 |
|
RU2196295C1 |
| 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 |
| GUIDED MISSILE AND SERVO UNIT FOR IT | 2000 |
|
RU2184927C1 |
| METHOD FOR CONTROL OF SPIN-STABILIZED MISSILE AND GUIDED MISSILE | 2000 |
|
RU2166727C1 |
| CONTROL SYSTEM UNIT FOR MISSILE LAUNCHED FROM TUBULAR GUIDE | 2023 |
|
RU2806773C1 |
| COLLAPSIBLE AIRFOIL | 2012 |
|
RU2492412C1 |
