Power Supply Systems (PSS) serve to provide required-quality uninterruptible power supply to satellite onboard equipment.
Main principle of PSS operation is generation, storage, conditioning and transmission of electrical power to the satellite
instrumentation. A typical PSS includes an electrical generator, i.e. a solar array, storage modules consisting of batteries
with service automatics, and control, regulation, monitoring instrumentation.
- Uninterruptible power supply; - Independent functioning in a satellite with no maintenance required;
- High reliability and long operational life; - Adaptation to any satellite application;
- Advanced highly effecient power sources and storages.
- Wide range of power supply capabilities, from dozens of Watts to several kiloWatts; - Various nominal input voltages;
- High quiality and relatively low cost of generated power; - Full status diagnostics; - LEO thru GEO operational capability;
- Automated preoperation cycle.
| Current | Direct |
| Output voltage, V |
unstabilized 24…34. stabilized 27±2%, 110±3%. Stabilized Voltage Grid:±5, ±12, ±15 |
| Output power, W | from 10W to 15 kW |
| Performance factor | 0.8…0.95 |
| Failure-free operation probability | 0.98 |
| Lifetime | up to 15 years |
| Power generator | Solar arrays with silicon (Si) or gallium arsenide (GaAs) cells |
| Power storage |
Nickel Cadmium (NiCd), Nickel-Metal-Hydride (NiMH), Nikel Hydrogen (NiH), Lithium(Li) batteries |
| Control, regulation, monitoring instrumentation | Advanced aerospace circuit technology with microprocessors |
| Application | Microsatellites, remote-sensing satellites, communication satellites, space platforms, etc. |
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