FIELD: electricity.
SUBSTANCE: electric power supply system of space vehicle consists of solar battery, voltage stabiliser, storage battery, external power control; at that, voltage stabiliser of solar battery and discharge device of storage battery are made in the form of bridge inverters with common transformer; at that, input of charging device is connected to output winding of transformer; to the other output windings of transformer there connected are load feed devices with their own ratings of output voltage of alternating or direct current; at that, one of load feed devices is connected to stabiliser of solar battery and to discharge device of storage battery.
EFFECT: enlarging the possibilities of electric power supply system of space vehicle, improving output voltage quality, reducing development and manufacturing costs, reducing the time required for the system development.
1 dwg
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Authors
Dates
2010-08-10—Published
2009-06-29—Filed