FIELD: rocket engineering.
SUBSTANCE: invention relates to rocket and space equipment, namely, to apparatuses used at the stage of ground-based thermal-vacuum testing of CubeSat-standard satellites. Stand for thermal-vacuum testing of CubeSat-standard satellites of 1U to 12U formats comprises a vacuum chamber, a solar emission simulator, and a swing apparatus. The swing apparatus provides simultaneous rotation around and movement along its own axis, has a replaceable basket for loading into the chamber of the spacecraft. The chamber is additionally equipped with a flange with an observation window allowing for visual monitoring of the movement of the spacecraft, and an optical communication interface based on spaced optocouplers, combined with the swing apparatus.
EFFECT: simplified installation of the spacecraft on the swing apparatus.
1 cl, 3 dwg
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