FIELD: jet-propelled ammunition. SUBSTANCE: folding wing of a small-sized rocket has a base rigidly fastened on the rocket body and provided with a recess, blade with a mating fitting section hinge-joined to the movable inserts, as well as an unfolding device. The unfolding device is made in the form of a compound spring located in the base recess, rigidly fastened in its middle part and engageable with the inserts by its ends. EFFECT: reduced overall dimensions and mass of the rocket. 5 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| MISSILE FOLDING WING | 2005 |
|
RU2288434C1 |
| MISSILE FOLDING WING | 2007 |
|
RU2344364C1 |
| FOLDING WING OF AIRCRAFT | 2006 |
|
RU2336489C2 |
| MISSILE | 2005 |
|
RU2284458C1 |
| COLLAPSIBLE AERODYNAMIC MEMBER | 2001 |
|
RU2197704C1 |
| AERODYNAMIC CONTROL SURFACE (VERSIONS) | 2000 |
|
RU2184342C2 |
| METHOD OF OPENING CONTROL SURFACES OF GUIDED PROJECTILE ACTUATOR UNIT AND ACTUATOR UNIT FOR REALIZATION OF THIS METHOD | 2002 |
|
RU2237598C2 |
| FOLDING AERODYNAMIC MEMBER OF GUIDED PROJECTILE | 2004 |
|
RU2280230C1 |
| ARTILLERY SHELL | 2000 |
|
RU2172926C1 |
| UNIT OF STEERING DRIVE OF ARTILLERY SHELL | 2000 |
|
RU2175431C1 |
Authors
Dates
2002-06-27—Published
2001-04-05—Filed