the invention relates to space technology and is designed for long-term experiments in the conditions of outer space.the device contains a section 2 with the payload module 6, section 3 with the module power supply system 7 and module of management system of ship and equipment u0440u0438u0435u043du0442u0430u0446u0438u0438 8, section 4 with a module system of traffic management center of gravity and calibration 9 and aerodynamic surface 5.the device can ensure the long-term technological experiments on low earth orbit, with the expansion of the functional possibilities.
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