FIELD: rocketry.
SUBSTANCE: the rocket launcher has a flow-type launching tube coupled to the carrier and a circular cavity made on the inner surface of the tube near its rear end face. The circular cavity is filled with water. Water is in a shell made of material readily destructible by a gas jet, for example, polyethylene.
EFFECT: reduced gas dynamic action on the carrier at rocket launching due to interaction of gas jet with water.
3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| ROCKET LAUNCHER | 2007 |
|
RU2345309C1 |
| ROCKET LAUNCHER | 2009 |
|
RU2395053C1 |
| ROCKET LAUNCHER | 2011 |
|
RU2453789C1 |
| MISSILE LAUNCHING PLANT | 2013 |
|
RU2519606C1 |
| DEVICE FOR MISSILE LAUNCHING | 2012 |
|
RU2495353C1 |
| MISSILE LAUNCHING PLANT | 2014 |
|
RU2545154C1 |
| ROCKET LAUNCHER | 2015 |
|
RU2577605C1 |
| ROCKET LAUNCHER | 2009 |
|
RU2392572C1 |
| MISSILE LAUNCHING PLANT | 2014 |
|
RU2545155C1 |
| DEVICE FOR LAUNCHING MISSILES | 2011 |
|
RU2460028C1 |
