FIELD: jet-propelled armament. SUBSTANCE: the salvo-fire jet-propelled system has a launcher with a bank of launching tubes and jet projectiles positioned in the launching tubes. Each projectile is provided with an attitude control system. The bank of launching tubes in provided with a system for determining its attitude connected to the control system of each jet projectile via the information transmission channel and adjusted to the longitudinal axis of one of the launching tubes. The control system of each jet projectile is made for determining its angular deviation from the position of this axis. EFFECT: enhanced close grouping of shots and efficiency of target hitting at distances above 60 km. 1 dwg
Title | Year | Author | Number |
---|---|---|---|
SALVO LAUNCHING COMPLEX | 1998 |
|
RU2126945C1 |
SALVO JET PROJECTILE LAUNCHER | 1998 |
|
RU2126126C1 |
ROCKET PROJECTILE LAUNCHED FROM LAUNCHING TUBE | 1997 |
|
RU2115882C1 |
TAIL PLANE STABILIZER OF SUPERSONIC JET PROJECTILE | 2001 |
|
RU2176066C1 |
JET PROJECTILE | 2002 |
|
RU2220399C1 |
ROCKET MISSILE | 2006 |
|
RU2343397C2 |
SPIN-STABILIZED SUPERSONIC MISSILE | 2000 |
|
RU2166178C1 |
AERODYNAMIC STABILIZER OF SALVO-FIRE JET PROJECTILE | 2006 |
|
RU2313761C1 |
ROCKET | 1998 |
|
RU2125701C1 |
ROCKET | 1998 |
|
RU2125704C1 |
Authors
Dates
2001-06-10—Published
1999-12-20—Filed