DEVICE FOR FIXING CONTROLLED ROCKET Russian patent published in 2017 - IPC F41F3/04 

FIELD: engines and pumps.

SUBSTANCE: device for fastening a guided missile equipped with a starting engine in a transport-launch container (TLC) is made in the form of a cage. The cage consists of two pairs of semirings, the internal semirings being installed in the groove of the starting motor housing, the outer semirings are installed in the inner semirings groove and interact with the groove of the trapezoidal section on the inner surface of the TLC pipe. At the outer semirings junction, the L-shaped locking plates are fastened to the back cover of the container. On the body of the starting motor between its outer diameter and the diameter of the annular groove, two symmetrically located grooves are made on the length from the rear end of the starting motor to the annular groove. On each inner semiring, there are two symmetrically arranged ledges interacting with the locking plates and a protrusion cooperating with the corresponding groove on the housing of the starting motor.

EFFECT: increased reliability due to the exclusion of the rocket's turning on the roll in the transport-launch container during its operation.

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