FIELD: rocketry.
SUBSTANCE: rocket launcher comprises connected with carrier launching flow pipe with a bottom edge. On the starting flow pipe there is a toral tank with a dispersing medium. Toral tank is connected via pipelines through inlet control valves with circular row of drainage radial holes made in the side surface of the starting flow pipe at its bottom section and uniformly located along the perimeter of the starting flow pipe.
EFFECT: technical result is reduction of gas-dynamic action start shock wave at carrier rocket and high reliability of starting device.
1 cl, 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| ROCKET LAUNCHER | 2015 |
|
RU2577605C1 |
| MISSILE LAUNCHING PLANT | 2014 |
|
RU2545154C1 |
| MISSILE LAUNCHING PLANT | 2013 |
|
RU2519606C1 |
| ROCKET LAUNCHER | 2013 |
|
RU2516785C1 |
| DEVICE FOR ROCKET LAUNCHING | 2004 |
|
RU2275578C1 |
| ROCKET LAUNCHER | 2005 |
|
RU2295689C1 |
| ROCKET LAUNCHER | 2009 |
|
RU2395053C1 |
| DEVICE FOR MISSILE LAUNCHING | 2012 |
|
RU2495353C1 |
| METHOD FOR REDUCING GAS-DYNAMIC INFLUENCE ON GROUND OF START POSITION AND LAUNCHING STATION OF STARTING MISSILE JET STREAM AT ANGLES CLOSE TO VERTICAL ANGLE AND DEVICE FOR ITS IMPLEMENTATION | 2012 |
|
RU2481540C1 |
| MISSILE LAUNCHING PLANT | 2014 |
|
RU2545155C1 |
