FIELD: space industry.
SUBSTANCE: invention relates to the launching into orbits of an ensemble of artificial earth satellites (hereinafter – AES), mainly of pico-class. The distribution of AES into orbits is carried out by means of a transport spacecraft (hereinafter – TSC) containing satellite platform (2) maneuvering using propulsion system (9). TSC is launched into the initial orbit by a carrier rocket. In cargo compartment (12a) of platform (2), AES (12) are stacked, which are sequentially released from this compartment using a tube-shaped picosatellite orbital deployer (POD). The release of each AES (12) from cargo compartment (12a) occurs with the specified direction and speed when TSC reaches the corresponding point of its trajectory and orientation.
EFFECT: rapid deployment of small AES (such as Cubesat) with the required accuracy and relatively simple unified means.
9 cl, 8 dwg
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