FIELD: aircraft; rocket engineering.
SUBSTANCE: invention relates to aircraft and rocket engineering and can be used for aircraft compartment separation. Aircraft compartment separation system comprises a device for fastening a compartment to the aircraft along the junction frames, which is capable to release fastening, and a separation unit mounted on the aircraft and equipped with a pusher. Pusher contacts the thrust element of the compartment. On the junction frame of the compartment there is a landing belt for the aircraft junction frame. Composition of the separation device is enclosed by the enclosing shell with the front and rear flange fixed on it. Front flange of the shell is fixed to the end of the pusher, the rear flange is installed in the central hole of the junction frame of the compartment with the possibility of abutment in the end of the landing belt, which is an abutting element of the compartment.
EFFECT: technical result of the invention is higher reliability of aircraft compartment separation.
5 cl, 5 dwg
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