FIELD: rocketry.
SUBSTANCE: the missile launcher has a flow-through launching tube coupled to the carrier, and a flow-through probe fastened in the tube low section. A powder gas flow swirler made in the form of guide coiled ribs located on the probe inner surface is installed in the probe. The rib ends are positioned in the probe outer.
EFFECT: enhanced degree of quenching of the elapsing jet and reduced gas dynamic action on the carrier at a missile take-off.
2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| ROCKET LAUNCHER | 2008 |
|
RU2371657C1 |
| DEVICE FOR ROCKET LAUNCHING | 2004 |
|
RU2275578C1 |
| REVOLVING ROCKET LAUNCHER | 2008 |
|
RU2371658C1 |
| DEVICE FOR MISSILE LAUNCHING | 2006 |
|
RU2313753C1 |
| ROTARY ROCKET LAUNCHER | 2007 |
|
RU2346224C1 |
| ROCKET LAUNCHER | 2009 |
|
RU2395053C1 |
| ROCKET LAUNCHER | 2009 |
|
RU2392572C1 |
| ROCKET LAUNCHER | 2011 |
|
RU2453789C1 |
| DEVICE FOR ROCKET LAUNCHING | 2005 |
|
RU2290590C1 |
| DEVICE FOR ROCKET LAUNCHING | 2004 |
|
RU2275579C1 |
