FIELD: weapons and ammunition.
SUBSTANCE: proposed device comprises launching tube and diffuser moving axially relative to each other. Launching tube 1 is connected with carrier 2. Launching tube inner surface 5 has circular groove made in tube outlet cross section 3. Said groove forms circular cavity 7 when launching tube is jointed with diffuser. Said circular cavity 7 accommodates diaphragm 8.
EFFECT: increased attenuation of effused jet and reduced gas dynamic pressure on carrier in launching.
2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| ROCKET LAUNCHER | 2011 |
|
RU2453789C1 |
| ROCKET LAUNCHER | 2009 |
|
RU2392572C1 |
| ROCKET LAUNCHER | 2005 |
|
RU2295689C1 |
| MISSILE LAUNCHER | 2006 |
|
RU2318172C1 |
| ROCKET LAUNCHER | 2008 |
|
RU2371657C1 |
| ROCKET LAUNCHER | 2007 |
|
RU2345309C1 |
| ROCKET LAUNCHER | 2015 |
|
RU2577605C1 |
| MISSILE LAUNCHING PLANT | 2013 |
|
RU2519606C1 |
| ROCKET LAUNCHER | 2015 |
|
RU2577586C1 |
| DEVICE FOR ROCKET LAUNCHING | 2004 |
|
RU2275578C1 |
