FIELD: weapons and ammunition.
SUBSTANCE: device to increase flight distance comprises a body with a combustion chamber, a solid propellant charge, a bottom with nozzle holes, an igniter, a start-up mechanism, a supply unit, a voltage converter, a control unit, nozzle plugs, a pressure relay and a unit of fixation to the projectile. The solid propellant charge is installed in the combustion chamber. Nozzle plugs are installed in nozzle holes of the bottom. The unit of fixation to the projectile comprises electromagnets and a device cover. There are ledges provided on the end surface.
EFFECT: increased ballistic efficiency of a shot.
20 cl, 5 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD OF INCREASE OF RANGE CAPABILITY OF PROJECTILE (VERSIONS) AND DEVICE FOR ITS IMPLEMENTATION | 2010 |
|
RU2462686C2 |
| METHOD FOR FORMING A PROTECTIVE COATING OF GUN BARRELS | 2021 |
|
RU2769032C1 |
| METHOD OF INCREASING THE DISTANCE PLANE OF A CHARGER AND THE DEVICE FOR ITS IMPLEMENTATION (OPTIONS) | 2017 |
|
RU2647715C1 |
| METHOD FOR INCREASING THE FLIGHT RANGE OF ACTIVE-REACTIVE PROJECTILE AND ACTIVE-REACTIVE PROJECTILE WITH MONOBLOCK COMBINED ENGINE UNIT (VERSIONS) | 2020 |
|
RU2751311C1 |
| METHOD FOR INCREASING THE FLIGHT RANGE OF AN ARTILLERY PROJECTILE WITH A ROCKET-RAMJET ENGINE AND AN ARTILLERY PROJECTILE IMPLEMENTING IT (OPTIONS) | 2022 |
|
RU2785835C1 |
| METHOD FOR INCREASING FLIGHT RANGE OF THROWN SHELL, AND DEVICE FOR ITS IMPLEMENTATION | 2010 |
|
RU2457418C1 |
| ACTIVE-JET PROJECTILE WITH ROCKET-RAMJET ENGINE FOR GUNS WITH A RIFLED BARREL | 2018 |
|
RU2711208C1 |
| REACTIVE METAL DEVICE | 2018 |
|
RU2680568C1 |
| METHOD OF INCREASING THE DISTANCE OF THE ROCKET-PROPELLED GRENADE | 2017 |
|
RU2647256C1 |
| GUIDED MISSILE SOLID-PROPELLANT ROCKET ENGINE, SOLID PROPELLANT IGNITER AND ROCKET ENGINE NOZZLE ASSEMBLY | 2008 |
|
RU2351788C1 |
