FIELD: armament, in particular, rocketry.
SUBSTANCE: the folding aerodynamic unit of the guided missile has blades connected by an axle, and a spring. The blade tail section is positioned in a longitudinal groove of the axle, connected to it by a pin and provided with a bearing bevel. A spring-loaded stop bushing is loosely installed on the axle.
EFFECT: improved operating characteristics of the guided missile.
3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| FOLDING AERODYNAMIC CONTROL | 2005 |
|
RU2284450C1 |
| COLLAPSIBLE AERODYNAMIC MEMBER | 2001 |
|
RU2197704C1 |
| FOLDING AERODYNAMIC MEMBER OF GUIDED PROJECTILE | 2004 |
|
RU2280230C1 |
| METHOD OF OPENING CONTROL SURFACES OF GUIDED PROJECTILE ACTUATOR UNIT AND ACTUATOR UNIT FOR REALIZATION OF THIS METHOD | 2002 |
|
RU2237598C2 |
| COLLAPSIBLE AIRFOIL | 2012 |
|
RU2492412C1 |
| METHOD FOR CONTROL OF SPIN-STABILIZED MISSILE AND GUIDED MISSILE | 2000 |
|
RU2166727C1 |
| GUIDED MISSILE | 2003 |
|
RU2244897C1 |
| FOLDING AERODYNAMIC ROCKET RUDDER | 2023 |
|
RU2803760C1 |
| GUIDED PROJECTILE | 2001 |
|
RU2196295C1 |
| BLOCK OF THE CONTROL SYSTEM OF A ROCKET LAUNCHED FROM A TUBULAR GUIDE | 2022 |
|
RU2795712C1 |
