FIELD: rocket technology.
SUBSTANCE: invention relates to the field of rocket technology, and more specifically to the separation system. The rocket compartment separation unit includes power attachment units for the frames of the separated compartments, pyrolysis units for the power attachment units’ lock release and the compartment pusher. The pyrolysis unit for the power attachment units’ lock release is installed in a movable flange and is made in the form of a pneumatic cylinder with a piston that is shifted relative to the movable flange and the frame with a pusher of the compartment made on it. The pusher of the compartment passes through a cutout made in the frame, with an emphasis on the frame of another of the separated compartments.
EFFECT: increased reliability of the flyer is achieved.
1 cl, 6 dwg
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