FIELD: weapons.
SUBSTANCE: invention relates to the field of rocket equipment, and more specifically to the missile launching units. Device for orientation of rockets with elevation angle on launcher mounted on carrier, comprises adapters. Adapters are an intermediate link between launcher and launching pipes. Outer planes of the adapters on which the launching tubes are installed with their attachment elements are made with a slope outside from the plane of symmetry between the adapters. Slope of outer plane of adapter in cross-section by its plane, perpendicular to aiming line, is calculated by formula: 
α is angle of missiles divergence, ensuring their collision prevention during salvo firing; γ is the missile elevation angle, made structurally.
EFFECT: higher accuracy of firing.
1 cl, 4 dwg
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