FIELD: cosmonautics.
SUBSTANCE: invention relates to the load-bearing structure of a primarily modular artificial satellite and the node of junction thereof with the launch vehicle (carrier rocket). The load-bearing structure includes external closed panels (1) with internal reinforcements and corner beams (2) provided with detachable junctions (8) at the lower and upper edges thereof. Said junctions enable stacking of the satellite modules. Sliding panels (3) and horizontal panels (4) of the platform are installed inside the modules. The payload fitting (5) has detachable junctions (6) with beams (2) and a bolted junction (7) with the upper stage of the carrier.
EFFECT: increase in the efficiency of application of the satellite launch vehicle and increase in the internal volume of the satellite.
4 cl, 11 dwg
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