FIELD: electrical equipment of spacecrafts.
SUBSTANCE: invention relates to electrical equipment of spacecrafts (SC), in particular to connecting assemblies of solar panels, including flexible cable sections, which are subject to torsion during mutual movement of parts (panels) of SC. According to the invention, in the section passing through the hinge, cable conductors with considerable mutual potential difference (up to 100 V) are spaced from each other, besides, conductors with close potential are combined into bundles (trunks). This makes it possible to reduce the risk of insulation breakdown, which is damaged, in particular, by flows of charged cosmic particles.
EFFECT: increasing the reliability of the spacecraft's onboard electrical network.
2 cl, 2 dwg
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