FIELD: weapons and ammunition.
SUBSTANCE: missile launching plant includes a flow launching tube with front and rear end faces and connected to a carrier, an exhaust deflector in the form of a jet control element of reduction of gas-dynamic action, which is installed on the carrier tangentially to its surface.
EFFECT: invention allows reducing force impact of blast wave on the carrier at missile launching.
2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| ROCKET LAUNCHER | 2015 |
|
RU2577605C1 |
| MISSILE LAUNCHING PLANT | 2014 |
|
RU2545154C1 |
| DEVICE FOR MISSILE LAUNCHING | 2012 |
|
RU2495353C1 |
| MISSILE LAUNCHING PLANT | 2014 |
|
RU2545155C1 |
| ROCKET LAUNCHER | 2005 |
|
RU2295689C1 |
| DEVICE FOR ROCKET LAUNCHING | 2004 |
|
RU2275578C1 |
| ROCKET LAUNCHER | 2008 |
|
RU2371657C1 |
| ROCKET LAUNCHER | 2015 |
|
RU2577586C1 |
| DEVICE FOR LAUNCHING MISSILES | 2011 |
|
RU2460028C1 |
| DEVICE FOR ROCKET LAUNCHING | 2004 |
|
RU2275579C1 |
