FIELD: armament.
SUBSTANCE: the supersonic jet projectile has a tapered nose, cylindrical body and a blade tail unit. The center of gravity of the tail unit blade is shifted relative to the bottom shearing of the jet projectile in the direction of the conical section by a value determined according to the dependence. The aerodynamic chord of each blade of the tail unit is apart from the generating line of the cylindrical body by a value determined according to a dependence.
EFFECT: enhanced range of fire, reduced projectile dispersion.
1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| SUPERSONIC MISSILE | 2022 |
|
RU2799901C1 |
| ROTATING MISSILE | 2020 |
|
RU2732370C1 |
| ROTARY JET PROJECTILE | 2011 |
|
RU2451902C1 |
| SUPERSONIC JET MISSILE | 2007 |
|
RU2357193C1 |
| SUPERSONIC PROJECTILE | 2016 |
|
RU2642693C2 |
| ROCKET PROJECTILE | 2005 |
|
RU2288433C1 |
| SUPERSONIC CONTROLLED PROJECTILE | 2011 |
|
RU2459177C1 |
| ARTILLERY SHELL | 1998 |
|
RU2130581C1 |
| ROCKET PROJECTILE | 2004 |
|
RU2258890C1 |
| SUPERSONIC SPINNING MISSILE | 2010 |
|
RU2442101C1 |
