FIELD: rocketry, applicable in small-sized rockets launched from a transport-launching pack.
SUBSTANCE: in the guiding device for rocket launching the supports hinge-joined on the rocket body are made in the form of plate springs engageable with the tube inner surface. The front edges of the plate springs are made with a bevel towards the rear edge and with a rounding-off over the entire length. Radial flares toward the rocket body are made on the free ends of the springs, and shoulders filled with an elastic material are made in the perimeter of the recess on the side of the tube inner surface.
EFFECT: simplified device on the whole at simultaneous reduction of radial and longitudinal disturbances of the rocket and plant.
5 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| GUIDING DEVICE FOR ROCKET LAUNCHING | 1996 |
|
RU2114369C1 |
| GUIDING DEVICE FOR MISSILE LAUNCHING | 2004 |
|
RU2246679C1 |
| DEVICE TO SPIN MISSILE ALONG ROLL | 2008 |
|
RU2367879C1 |
| ROCKET IN LAUNCHING MATRIX | 2000 |
|
RU2191981C2 |
| METHOD OF MISSILE LAUNCH FROM CONTAINER AND DEVICE FOR ITS IMPLEMENTATION | 2006 |
|
RU2334192C2 |
| MECHANISM OF MISSILE RETAINING IN LAUNCHING CONTAINER | 2005 |
|
RU2284000C1 |
| TWO-STAGE MISSILE IN LAUNCHING PACK | 2005 |
|
RU2302600C1 |
| MECHANISM FOR RETAINING OF MISSILE IN LAUNCHING PACK | 2004 |
|
RU2265182C1 |
| ROCKET IN LAUNCHING PACK | 2002 |
|
RU2238515C2 |
| CONTAINERISED ROCKET | 2006 |
|
RU2329458C1 |
