FIELD: aviation.
SUBSTANCE: method for spacecraft (SC) manufacturing includes assembling of the spacecraft comprising a power supply system with solar panels, batteries and a stabilized voltage converter with a common bus connected with the spacecraft body after the spacecraft checkout. Increased current flow technical protection devices are installed to the break in the common bus and the spacecraft power supply system communication circuit for the period of the spacecraft manufacturing. In the process of the spacecraft manufacturing for different stages of treating it, the value of the increased current for actuation of the protection devices is set individually. Protection from the flow of increased current in the technical protection devices is provided by parallel connection of fuses to the required total value of the operating current. Break of the fuses electrical circuit is accompanied by signals generation.
EFFECT: provided fail-free spacecraft manufacturing process.
2 cl, 1 dwg
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Authors
Dates
2018-06-08—Published
2016-07-01—Filed