POWER SUPPLY SYSTEM OF SPACECRAFT WITH EXTREME SOLAR BATTERY POWER CONTROL

摘要

FIELD: astronautics.;SUBSTANCE: power supply system of a spacecraft comprises a solar battery (SB), a current sensor, a digital control system with an emergency SB power controller, voltage regulator made in form of bridge inverter with input C-filter, transformer with primary and secondary windings, two rectifiers, charging degree control device, a charging device, an accumulator battery, a discharge device, a load, a supply and control system, a stationary plasma engine.;EFFECT: higher specific energy efficiency, higher efficiency of energy transfer, reduced weight of additional energy converters.;1 cl, 2 dwg