FIELD: weapons and ammunition.
SUBSTANCE: invention relates to weapons, namely to jet ammunition. Rocket-assisted projectile launches from launching tube, plugged from bottom part. Projectile comprises rocket part with channel mid-flight charge, igniter and nozzle unit, gas generator with additional charge of bag charging, initiator. Initiator is installed in end of gas generator housing and connected via gas duct with afterburner tube. Augmenter tube passes through bag and central nozzle and directed to igniter through channel cruise charge. Gas generator is fixed on nozzle unit and has calibration undercuts on housing belt.
EFFECT: higher reliability of initiation and efficiency of unguided jet projectile.
1 cl, 1 dwg
Title | Year | Author | Number |
---|---|---|---|
PROJECTILE SEPARATION COMPARTMENT | 2015 |
|
RU2593851C1 |
ROCKET | 1998 |
|
RU2134860C1 |
ROCKET ENGINE OF ROCKET-ASSISTED PROJECTILE | 2016 |
|
RU2620613C1 |
SOLID-PROPELLANT ROCKET ENGINE | 1995 |
|
RU2111372C1 |
METHOD FOR LAUNCHING OF JET PROJECTILE AND COMPLEX OF FACILITIES REALIZING IT | 2000 |
|
RU2167385C1 |
GUIDED MISSILE SOLID-PROPELLANT ROCKET ENGINE, SOLID PROPELLANT IGNITER AND ROCKET ENGINE NOZZLE ASSEMBLY | 2008 |
|
RU2351788C1 |
METHOD OF INCREASE OF RANGE CAPABILITY OF PROJECTILE (VERSIONS) AND DEVICE FOR ITS IMPLEMENTATION | 2010 |
|
RU2462686C2 |
CUMULATIVE-HIGH-EXPLOSIVE CHARGE ENGINE | 2018 |
|
RU2675983C1 |
ROCKET | 2005 |
|
RU2293283C1 |
SMOKE GRENADE | 2007 |
|
RU2354920C2 |
Authors
Dates
2016-08-20—Published
2014-12-01—Filed