FIELD: aviation.
SUBSTANCE: connectivity device of space vehicle separated elements contains a docking fitting and a detachable fitting. Fittings are located on the joint plane, through holes of which a pyrobolt with a fixing nut and a flat washer is installed. The device is further provided with a curved plate. One end of the plate is rigidly fixed to the detachable fitting by means of the fixing unit, and the other is in contact with the fixing nut and is provided with a hole through which the threaded portion of the pyrobolt is passed. A flat washer is rigidly connected to a detachable fitting. Pyrobolt is made in two diameters d>d1 with a ledge located between the joint plane and the flat washer, with the possibility of interaction of this ledge with a flat washer in the course of operation.
EFFECT: improved performance of the connectivity device.
2 cl, 2 dwg
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