FIELD: transport.
SUBSTANCE: invention relates to aerospace engineering. Proposed process consists in assembly of spacecraft, electric tests for serviceability, tests for sustaining the mechanical effects and thermal vacuum tests performed in a definite way. Prior to mechanical tests, capacity of storage batteries is calculated, standard storage batteries are charged to total magnitude exceeding the design magnitude. In case design total capacity of storage batteries operation term is divided into parts to satisfy the requirements of design capacity. Initial state of electric power supply is checked up and maintained.
EFFECT: functional reliability of spacecraft fabrication.
3 cl, 1 dwg
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Authors
Dates
2015-10-20—Published
2013-12-09—Filed