FIELD: astronautics.
SUBSTANCE: invention relates to aerospace engineering, particularly, to rocket launching. Proposed method comprises vertical launching of rocket from launching container arranged on air carrier. "Cold" start of the missile is used with the help of a catapulting or obturator device. Delayed start of gas-dynamic system of transverse stabilization and declination of missile for time sufficient for output of nozzle device of gas-dynamic transverse system of stabilization and declination of missile from launching container into air. Delayed launching of sustainer rocket engine.
EFFECT: simplified design of carrier.
1 cl, 1 dwg
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