FIELD: weapons.
SUBSTANCE: invention is related to missilery and may be used in designs of antihail, meteorological and other missiles having parachute system that provides for termination of flight that is safe for public and economic objects. Missile head comprises head fairing installed on missile body with the help of interlock, parachute system installed inside fairing, and pyrotechnic expelling device with flow unit. Inside head fairing there is tube rigidly installed, which interacts with external surface with cylindrical shell arranged on missile body. Flow unit of expelling device is connected to internal cavity of tube. Parachute system shrouds are fixed in missile body with the help of swivel.
EFFECT: improved functional-operating characteristics of missile by means of its design simplification, cost reduction and increase of reliability.
2 cl, 2 dwg
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Authors
Dates
2009-05-10—Published
2007-10-10—Filed