FIELD: power supply systems.
SUBSTANCE: used in the design and creation of spacecraft (SC) power supply systems. The system contains a group of solar panels electrically connected to a voltage stabilizer, a charger, a battery and a group of consumers, as well as a discharge device electrically connected to a charger, a battery, a voltage stabilizer and a group of consumers, the battery being electrically connected to a battery charge controller having electrically connected switching devices and batteries. At the same time, the battery charge controller is electrically connected to the positive and negative buses of groups of one or more sectioned piezoelectric generators and rectifiers mounted on the inner surfaces of the shell walls of the launch vehicle stages.
EFFECT: compensation for the loss of electricity to keep the spacecraft propulsion engine in a neutral position in the process of orbit insertion.
1 cl, 2 dwg
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Authors
Dates
2023-04-20—Published
2022-10-21—Filed