FIELD: armament.
SUBSTANCE: the mechanism for retaining of missile in the launching pack has a threaded ring fixing it in the launching pack by means of a thrust bush, shutter engageable by the free end with the rear cover of the pack, and a spring ring with radial grooves and shoulders in the point of joint, installed on the missile engine between the rear end of the pack and the end surface projecting from it. The thrust bush is made in the form of a ring thrust with radial slots on the end, in which the upper part of the shutter is hinge-fastened. The shoulders of the slot spring ring are positioned inside the groove with a clearance relative to its side walls, and its inner diameter is made proceeding from the provision of engagement with the groove bottom.
EFFECT: provided use of the mechanism for retaining of missile in the launching pack in missiles with engine nozzle units of different types.
4 dwg
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Authors
Dates
2005-11-27—Published
2004-11-04—Filed