FIELD: cosmonautics.
SUBSTANCE: invention relates to design and equipment of spacecrafts (SC). Housing of the proposed platform is a leaky compartment in the form of a rectangular parallelepiped. Housing consists of bearing side panels (1), base side boards (2), end panel (3), end base board (4), and docking bracket (5). Platform also contains the necessary units of onboard equipment (6) and solar batteries (7). Base boards (2, 4) are multilayer printed-circuit boards from fibreglass laminate, on the outer surface of which a temperature-regulating coating is applied to release heat into space. Basic boards (2, 4) are an alternative to the on-board cable network and are intended for switching of all units of on-board equipment (6) of the spacecraft. Basic boards are equipped with connectors (8) for connection of onboard equipment (6), connectors (9) providing communication between all basic boards, as well as built-in solar sensors (10) and magnetometers (11).
EFFECT: shorter time for using the on-board cable network, as well as time for assembling the entire spacecraft.
1 cl, 6 dwg
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Authors
Dates
2024-08-21—Published
2024-01-31—Filed