FIELD: aerospace industry.
SUBSTANCE: invention relates to devices for rotary ascent devices (RAD) of space objects (SO) and their groupings into given orbits or for their delivery to the surface of the Earth and other celestial bodies. The speed required for this is achieved by rotating the SO together with the RAD around their common center of mass and separating from the RAD with a given throwing angle. SOs can additionally rotated relative to any associated axes of the RAD. The latter is equipped with sensors for determining the angles of orientation of the axis of rotation of the rotated and a device for imparting rotation to it relative to this axis. SO ejection devices, for example, spring type, can have magazines.
EFFECT: expanding the composition of space assets capable of solving the specified tasks of SO ascent, including those stabilized by rotation, in the process of their normal operation.
2 cl, 4 dwg
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