FIELD: rocketry, in particular, devices for rocket launching.
SUBSTANCE: the device for rocket launching hasa flow-through launching tube linked with the carrier, and a flow-through probe fastened on the rear section of the tube. Radial slots that a flow-through in the longitudinal direction are made on the inner surface of the flow-through probe.
EFFECT: reduced gas dynamic action on the carrier.
3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| ROCKET LAUNCHER | 2008 |
|
RU2371657C1 |
| MISSILE LAUNCHER | 2006 |
|
RU2318172C1 |
| ROCKET LAUNCHER | 2015 |
|
RU2577605C1 |
| DEVICE FOR MISSILE LAUNCHING | 2006 |
|
RU2313753C1 |
| ROTARY ROCKET LAUNCHER | 2007 |
|
RU2346224C1 |
| REVOLVING ROCKET LAUNCHER | 2008 |
|
RU2371658C1 |
| DEVICE FOR MISSILE LAUNCHING | 2012 |
|
RU2495353C1 |
| DEVICE FOR ROCKET LAUNCHING | 2005 |
|
RU2290590C1 |
| DEVICE FOR ROCKET LAUNCHING | 2004 |
|
RU2275579C1 |
| ROCKET LAUNCHER | 2013 |
|
RU2516785C1 |
