FIELD: armament.
SUBSTANCE: the guided missile has a detachable zero stage, sustainer stage with nose cone, nose air intake, body with air-dynamic control actuator and aerodynamic controls. The sustainer stage of the missile uses a heat-exchange device, whose input is connected to the input of the air intake, and the output - to the input of the gas distributing device of the control actuator.
EFFECT: enhanced reliability of the guided missile.
5 dwg, 1 ex
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Authors
Dates
2005-08-20—Published
2004-06-28—Filed