FIELD: ammunition for antipersonnel automatic and subcaliber hand rocket launchers, in particular, tail assemblies of high-explosive warheads. SUBSTANCE: the tail assembly for warheads of artillery cartridges, whose caliber is commensurable with the burner cup of rocket launcher barrel at a guaranteed minimum clearance, has a power filling combustion chamber fastened to the warhead body, limited by a gasket from the top representing a profiled plate spring installed inside the combustion chamber, closed from the end with a diaphragm carrying a percussion primer and covered with a membrane. The combustion chamber is provided inside with a step of smaller diameter for press-fitting of the gasket, and from the outside it has minimum two annular tapered undercuttings inclined to the side opposite the diaphragm. EFFECT: provided rational use of the propelling impulse for stabilization of the ballistic characteristics of the artillery cartridge warheads. 2 dwg
| Title | Year | Author | Number | 
|---|---|---|---|
| ASSEMBLED CARTRIDGE CASE | 2001 | 
 | RU2206860C1 | 
| SHELL AND CASE OF A GRENADE LAUNCHERS | 2003 | 
 | RU2235273C1 | 
| PROPELLANT CHARGE FOR GRENADE | 2023 | 
 | RU2812499C1 | 
| ARTILLERY ROUND FOR ROCKET LAUNCHER | 1998 | 
 | RU2125226C1 | 
| ARTILLERY CARTRIDGE FOR GRENADE LAUNCHER | 2004 | 
 | RU2282130C1 | 
| ARTILLERY CARTRIDGE | 2010 | 
 | RU2421685C1 | 
| PRACTICE ROUND | 2006 | 
 | RU2326334C1 | 
| RIFLE-ATTACHED GRENADE LAUNCHER ROUND | 2007 | 
 | RU2342625C1 | 
| GRENADE LAUNCHER ROUND | 2007 | 
 | RU2347176C2 | 
| ROUND FOR GRENADE LAUNCHER | 2013 | 
 | RU2525352C1 | 
Authors
Dates
2003-07-27—Published
2001-11-15—Filed