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