FIELD: guided missiles, applicable in the constructions of anti-tank missiles launched from launching packs with low initial speeds.
SUBSTANCE: the wire communication line in the tail section of the guided missile is made in the form of a control microcable wound on the body of the booster engine. The inner end of the microcable connected to the control compartment. Installed on the body of the booster engine is a protective screen protecting the control microcable against damage at ignition of the tracer pyrotechnic compound. The height of the protective screen is commensurable with the height of the control cable winding, and its area exceeds the tracer burning area formed during the time period from the moment of launching to deployment of the stabilizers.
EFFECT: enhanced adaptability to manufacture, strength, electric insulation and operating characteristics of the rocket, and simplified construction of it.
2 dwg
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Authors
Dates
2005-02-27—Published
2003-07-02—Filed