FIELD: astronautics.
SUBSTANCE: invention relates to space engineering, particularly, to creation of spacecrafts. Proposed method comprises power supply system including solar batteries, accumulator batteries and stabilized voltage converter and consists in assembly of electric circuits. After said operations, SC is subjected to electric tests for functioning, tests for mechanical loads, thermovacuum tests, as well as final tests. Final tests are carried out with power of spacecraft from accumulator batteries. Voltages of the stabilized voltage sources are controlled until appeared corresponding charging currents decrease to the minimum set value, after which the levels of limitation of values of currents of sources of stabilized voltage are increased to the required value.
EFFECT: reduced time of spacecraft manufacturing.
1 cl, 1 dwg
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Authors
Dates
2020-03-11—Published
2019-01-10—Filed