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A selection of completed and ongoing engineering programmes across power electronics, defence avionics, RF systems, and embedded platforms. All client details are protected under NDA.

Avionics Power Supply Unit for Fixed-Wing UAV
Delivered2024
Defence & Aerospace

Avionics Power Supply Unit for Fixed-Wing UAV

A MIL-grade multi-output power supply unit designed for a fixed-wing unmanned aerial vehicle operating in high-vibration, wide-temperature environments.

The Challenge

The client required a compact, high-reliability PSU delivering five isolated output rails from a 28 V DC bus, compliant with MIL-STD-704F and DO-160G. The unit had to survive 6g vibration, operate from -40°C to +85°C, and pass MIL-STD-461F EMI/EMC qualification.

Our Approach

We designed a phase-shifted full-bridge primary topology with synchronous rectification on all output rails. Magnetic components were custom-wound using high-temperature materials. The PCB was designed for conformal coating and potting. Thermal analysis was performed using CFD simulation before prototype build.

Outcome

The PSU passed all qualification tests on first submission — MIL-STD-461F, DO-160G vibration and thermal shock, and MIL-STD-704F input transient tests. Delivered on schedule with full test documentation.

Technical Specifications

Input Voltage

28 V DC (MIL-STD-704F)

Output Rails

5 isolated outputs

Power Output

120 W total

Efficiency

91% at full load

Temp Range

-40°C to +85°C

Standards

MIL-STD-461F, DO-160G

Keywords

DC-DC ConverterMIL-STD-704FDO-160GAvionicsUAV

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All projects shown here are presented with client permission or with identifying details removed. Client names, platform designations, and classified technical parameters are withheld in all cases. We do not disclose client identities without explicit written consent. Enquiries about specific programmes are handled under NDA.

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