FIELD: rocket engineering.
SUBSTANCE: invention relates to the field of rocket engineering, more specifically, to systems for releasing or separating objects of an aerial vehicle. System for separating rocket stages includes attachment fittings for frames of the separated structures, mounting surfaces made in the end planes of the frames, explosive units for releasing the attachment fittings, and a compartment pusher. The attachment fittings for the frames comprise thrust flanges made on the frame of one of the separated structures and locking levers made on the frame of the other one of the separated structures, installed on the axes of rotation. Also provided is a movable frame installed on guides through the windows made in the movable frame, configured to be moved along the guides, locks for the final position of the movable frame, rods connecting the movable frame with opposing parts of the locking levers. The locks for the final position of the movable frame are made on the guides in the form of deformable locking cones blocking the movable frame when the frame is moved to the end position. The thrust flanges and thrust ends of the locking levers are made at an angle to the mounting plane of the frames.
EFFECT: structural simplification.
1 cl, 6 dwg
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Authors
Dates
2022-05-13—Published
2021-03-12—Filed