FIELD: space technology.
SUBSTANCE: invention relates to the field of rocket and space technology, and more specifically to undocking devices. The device for undocking rocket and space objects contains docking frames with a system of locks, pins, spring pushers, mechanical sensors for undocking control with spring-loaded rods. There are mechanisms for converting the movement of the rods of the undocking control sensors, including a sleeve fixed in one of the docking frames, open with one end towards the docking plane, as well as a finger placed inside the sleeve. Each of the undocking control sensors is installed in the docking frame in the area of the corresponding lock. The axis of the sensor is at an angle to the axis of the corresponding sleeve of the rod displacement conversion mechanism. A through hole is made in the side surface of the sleeve coaxially to the spring-loaded sensor rod. The spring-loaded sensor rod contacts its end face with the side surface of the finger. A flexible retaining element is attached to the end of the finger coming out of the sleeve with one side.
EFFECT: increased reliability is achieved.
3 cl, 11 dwg
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Authors
Dates
2021-11-12—Published
2020-09-02—Filed