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
| Title | Year | Author | Number | 
|---|---|---|---|
| POWER SUPPLY SYSTEM OF SPACE VEHICLE WITH POWER REGULATION OF SOLAR PANEL BY INVERTING-TRANSFORMER CONVERTER | 2014 | 
 | RU2574565C1 | 
| SPACECRAFT ELECTRIC POWER SUPPLY SYSTEM | 2015 | 
 | RU2613660C2 | 
| SPACECRAFT POWER SUPPLY SYSTEM WITH OPTIMISED CONTROL FOR SOLAR BATTERY POWER | 2014 | 
 | RU2560720C1 | 
| SPACECRAFT POWER SUPPLY SYSTEM | 2018 | 
 | RU2680245C1 | 
| HIGH-VOLTAGE POWER SUPPLY SYSTEM OF SPACE VEHICLE | 2016 | 
 | RU2634513C2 | 
| SPACECRAFT POWER SUPPLY SYSTEM | 2016 | 
 | RU2653704C2 | 
| HIGH-VOLTAGE POWER SUPPLY SYSTEM OF SPACECRAFT | 2016 | 
 | RU2650100C1 | 
| HIGH-VOLTAGE POWER SUPPLY SYSTEM OF SPACE VEHICLE WITH INDUCTIVE-CAPACITIVE CONVERTER | 2016 | 
 | RU2634612C2 | 
| SPACECRAFT POWER SUPPLY SYSTEM | 2019 | 
 | RU2724111C1 | 
| METHOD TO CONTROL AUTONOMOUS POWER SUPPLY SYSTEM OF SPACECRAFT | 2014 | 
 | RU2572396C1 | 
Authors
Dates
2019-10-30—Published
2018-11-12—Filed