FIELD: weapons and ammunition.
SUBSTANCE: invention refers to military equipment and may be used for development of missile take-off from container. By specified impact zone and known direction of deviation, determined are a value and a sign of controls displacement angle, first-stage engine operation time, controls are rigidly fixed in zero position, mechanical stops are installed fixedly, tanks of dummy are fueled as required, energetic device of catapult launch is engaged, missile dummy is catapulted from container, an engine is started after the dummy coming from container with time delay relative to the moment of the dummy coming out from container, a tray is detached from the dummy, servo units rods controls are unlocked using constant electrical signal of specified polarity, controls are displaced and restrained to installed mechanical stops using servo units, displace the dummy from the launching facility to the specified impact zone.
EFFECT: providing non-use of control system for take-off and dummy displacement from take-off position.
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