FIELD: space engineering.
SUBSTANCE: invention is related to structures of space engineering and may be used in design of spacecrafts of various purposes. According to invention, spacecraft comprises truss-frame reinforced structure, body panels, target equipment and supporting systems. These systems include power supply system, which consists of solar and nickel-hydrogen accumulator batteries, and also complex of automatics and stabilisation of voltage. At the same time equipment of specified complex, or its part is installed inside bodies of nickel-hydrogen accumulator batteries.
EFFECT: increased density of aggregates and systems layout inside body of spacecraft, reduced length of communication lines between accumulator batteries and equipment of specified complex, and also increased security of on-board equipment against electromagnet noise.
1 dwg
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