FIELD: weaponry.
SUBSTANCE: invention relates to rocket production. Device comprises container with bottom chamber representing accumulator with solid propellant charge and pyro-igniter, obturator with seals fixed on the guided missile and to be separated there from at the missile flight end and obturator stops. In compliance with the invention, the proposed device differs in that the obturator represents piston attached to the guided missile tail part on the nozzle face and comprises central part extending in the missile engine nozzle. It also incorporates tight peripheral part bent towards the missile. Note here that the pressure source is fastened on the obturator central part and has its nozzle oriented towards the container bottom.
EFFECT: reduced damages of missiles assemblies due to ruling out effects of accumulator effluent gases.
4 cl, 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| GUIDED MISSILE LAUNCHING DEVICE | 1997 |
|
RU2114371C1 |
| DEVICE FOR LAUNCHING GUIDED MISSLE | 2016 |
|
RU2639839C1 |
| TRANSPORTING-LAUNCHING CONTAINER | 2008 |
|
RU2388984C1 |
| SMALL-SIZED GAS-DYNAMIC STEERING APPARATUS | 2020 |
|
RU2753034C1 |
| AUTOMATIC WEAPON WITH INNER PISTON FOR CASELESS CARTRIDGE | 2016 |
|
RU2669037C2 |
| SHIP-BORNE MISSILE STORAGE AND LAUNCHING PACK | 1999 |
|
RU2156941C1 |
| REVOLVER REMOTE ELECTRIC SHOCK WEAPON | 2022 |
|
RU2781908C1 |
| METHOD FOR INCREASING FLIGHT RANGE OF THROWN SHELL, AND DEVICE FOR ITS IMPLEMENTATION | 2010 |
|
RU2457418C1 |
| METHOD FOR REDUCING RECOIL FORCE OF FIREARMS AND GUN WITH FOLDING BARREL CHAMBER FOR IMPLEMENTATION THEREOF (EMBODIMENTS) | 2019 |
|
RU2736305C1 |
| IMPULSE-REACTION ENGINE | 1996 |
|
RU2132964C1 |
