FIELD: artillery ammunition. SUBSTANCE: the jet projectile has a nose section combined with the engine. The engine carries a fin with opening blades. The stabilizer casing is made in the form of a thin-walled cylinder consisting of spring blades rolled up in circumference and successively fastened to one another. Each blade is concave towards rolling-up, and the fin casing longitudinal axis is aligned with the projectile longitudinal axis. EFFECT: reduced passive weight of the projectile. 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| ROCKET | 1995 |
|
RU2103651C1 |
| ROCKET | 2000 |
|
RU2183816C2 |
| ROTARY JET PROJECTILE | 2011 |
|
RU2451902C1 |
| PROGECTILE | 2006 |
|
RU2309376C1 |
| HAND GRENADE LAUNCHER | 2000 |
|
RU2190179C2 |
| STABILIZING DEVICE | 1999 |
|
RU2153146C1 |
| FOLDING WING OF SMALL-SIZED ROCKET | 2001 |
|
RU2184339C1 |
| ARTILLERY SHELL | 2000 |
|
RU2172926C1 |
| ROCKET | 2001 |
|
RU2191983C1 |
| JET PROJECTILE WITH DETACHABLE ENGINE | 1999 |
|
RU2157505C1 |
Authors
Dates
2001-04-20—Published
2000-02-03—Filed