| 摘要 |
FIELD: rocket equipment, can be used in constructions of transport-launching containers for launching of small-sized rockets and antiaircraft missiles. SUBSTANCE: in the rocket launching device, using a cylindrical container, releasable front cover with the front collar hinge- joined to the container, rear cover, [provision is made on the inner side of the front cover for a locking device made in the form of a flat spring with a shaped deflector installed on it; one end of the spring is rigidly fastened to the inner side of the cover, and the other end carries a plate for movement in the cover guides and in the slot formed on the inner side of the container; the cover supporting collar is made flush with the cover external surface, and secured on the outer side of the cover symmetrically about the collar is a spring catch attached to the container housing by means of a detachable hinge joint; the side surface of the container cover has an annular groove receiving an elastic seal, and the outer side of the cover, in its center, has a stopper with a sealing component installed in a threaded hole; a nut is positioned on the flat spring of the locking device in the same axis with the stopper. The rocket launching device of such a design is intended for directional launch and protection of the rocket against mechanical damages, weather effect and biological pests in service, it functions as follows: while moving in the container, the rocket warhead touches the deflector, shifts it in the direction of motion making the flat spring sag. The flat spring sags and pulls the plate of the locking device moving it in the cover guides until it completely comes out of the slot in the container housing. The rocket continues its motion and acts on the front cover through the deflector and flat spring. Due to the summary force produced by the rocket and flat spring, the front cover turns on the axle of the detachable hinge joint, tips over, opens the container, and gets released. EFFECT: enhanced operating characteristics of the rocket due to reduced disturbing factors acting on the rocket at its launching from the launching container. |
