FIELD: military equipment, applicable for designing of recoilless guns. SUBSTANCE: the gun has a barrel, propelling charge, useful load and electric primers. The propelling charge is positioned in stages separated by partitions, each stage consists of combustion chambers separated by partitions, with propelling charges and electric primers located in them. The combustion chambers are connected by an electric circuit. The last of the combustion chambers serves as a locking device. The quantity of the stages may make up two and more. The replaceable stages may be made for their successive switching. EFFECT: enhanced shell velocity. 4 cl, 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| ENGINE FOR SHELLS OF RECOILLESS GUNS | 2002 |
|
RU2221978C2 |
| ENGINE FOR ARTILLERY SHELLS | 2002 |
|
RU2221977C2 |
| ROCKET FOR GRENADE LAUNCHED BY GRENADE LAUNCHER | 2002 |
|
RU2217618C1 |
| LONG-RANGE DIRECTIONAL-ACTION MINE | 2002 |
|
RU2221984C2 |
| STAGE ENGINE | 2002 |
|
RU2223411C2 |
| EXPLOSIVE TUBULAR BOOSTER | 2002 |
|
RU2221979C2 |
| TUBULAR BOOSTER | 2002 |
|
RU2219464C1 |
| TUBULAR BOOSTER | 2002 |
|
RU2219463C1 |
| TUBULAR BOOSTER | 2002 |
|
RU2219467C1 |
| TUBULAR BOOSTER | 2002 |
|
RU2219466C1 |
