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Power converter for aerospace applications Triton-X PCU
for satellite platformDC/DC

power converter for aerospace applications
power converter for aerospace applications
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Characteristics

Applications
for aerospace applications, for satellite platform
Type
DC/DC
Output voltage

28 V

Current

30 A

Description

The Power Conversion Unit (PCU) for a small satellite platform is single-failure-tolerant and based on GaN technology for power semiconductors. The solar array regulator stages operate with buck-boost regulators (B2R). TM/TC control is implemented via a CAN bus interface. Details: Mass: 4.5kg Volume: 5.6 liters Solar power input: 900W SAR principle: MPPT Efficiency >94% Output: 28V unregulated bus 30A max. Output power 450W Battery charge control majority voter Battery disconnect switch

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*Prices are pre-tax. They exclude delivery charges and customs duties and do not include additional charges for installation or activation options. Prices are indicative only and may vary by country, with changes to the cost of raw materials and exchange rates.