FIELD: military equipment, in particular, recoilles guns. SUBSTANCE: the propellant charge is positioned in combustion chambers formed by interchamber partitions. The means of initiation is made in the form of electric primers installed in the propellant charge. The combustion chambers are connected by an electric circuit. The combustion chamber that is the last to the outlet of the tube is designed for its dynamic locking. EFFECT: enhanced mass of the propelled body and range of its flight, as well as reduced mass and overall dimensions of the recoilless gun. 3 cl, 1 dwg
Title | Year | Author | Number |
---|---|---|---|
RECOILLESS GUN FOR SHELLS | 2002 |
|
RU2221980C2 |
ENGINE FOR SHELLS OF RECOILLESS GUNS | 2002 |
|
RU2221978C2 |
ROCKET LAUNCHER USING EXPLOSIVE TUBULAR BOOSTER | 2002 |
|
RU2217680C1 |
ENGINE FOR ARTILLERY SHELLS | 2002 |
|
RU2221977C2 |
MINE IN EXPLOSIVE TUBULAR BOOSTER | 2002 |
|
RU2217689C1 |
EXPLOSIVE TUBULAR BOOSTER | 2002 |
|
RU2217678C1 |
LONG-RANGE DIRECTIONAL-ACTION MINE | 2002 |
|
RU2221984C2 |
EXPLOSIVE TUBULAR BOOSTER | 2002 |
|
RU2221979C2 |
TUBULAR BOOSTER | 2002 |
|
RU2219463C1 |
TUBULAR BOOSTER | 2002 |
|
RU2219464C1 |
Authors
Dates
2003-12-20—Published
2002-04-12—Filed