FIELD: rocket engineering. SUBSTANCE: for increase of mobility and combat invulnerability of rocket complexes with ground or water-surface launching it is proposed to carry out preliminary tossing up of launcher with rocket into air with subsequent stabilization, turn and control over them and over exit of rocket from launcher. For realization of proposed method there are provided system of deflection of launcher with rocket from carrier, system of stabilization, turn and control over launcher with rocket. Proposed method and device for its realization make it possible to ensure launching of rocket under any angle to plane of horizon at initial position of launcher with rocket and independent of condition of surface where launching position is located. EFFECT: increased mobility and invulnerability of rocket complexes. 2 cl, 6 dwg
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