| 摘要 |
An appliance for rocket launching has hinged as a rectangle a body, a front (to the side of the rocket launching) terminal lever, a beam, a rear terminal lever and a lock in the body, this locks the units of the suspension of the rocket through fixation of the beam closely to the body in such way that the terminal levers are turned back. To secure opening of the lock of the appliance for rocket launching and more smooth separation of the rocket from the launching appliance, the mechanism for the lock opening is arranged as a lever hinged to the body, its free end at suspended rocket is behind the cut of its nozzle and can turn under effect of pressure of gas jet of its jet engine with unlocking by means of con-rod hinged to it the lock, and the terminal levers and the beam in the placed of hinged joint of those have in pairs cuts and/or slots to which the nodes of the suspension of the rocket go at its hinging, with fixation at approaches of the beam and the body. In each pair of such cuts and/or slots effect of discrepancy is used, this provides forced push-out of the suspension unit of the rocket from the beam at moving away the beam from the body under effect of driving force of the rocket engine at its launching.
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