FIELD: armaments and ammunition.
SUBSTANCE: invention can be used to separate and to jettison the payload fairing of the carrier missile. The device for separation and jettison of payload fairing of carrier missile with possibility of rotation, pushers supported by the carrier missile fittings, shank with spherical end edges, springs with opposite direction of winding, and installed one in another. The pusher contains telescopically connected with each other external cylinder with sleeve with rigidly connected bottom lid with small sleeve, and internal cylinder with rod with rigidly secured top lid with sleeve. The sleeves are telescopically connected with each other with cavity creation between the bottom and top lids.
EFFECT: invention improves reliability of separation and jettison of the payload fairing.
2 dwg
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