Power-system mass is a central design constraint for drones, UAVs and other weight-sensitive mobile platforms. The SydroPOWER Air™ KZ3000F is a drone-optimised, air-cooled hydrogen fuel cell system developed for projects requiring approximately 3 kW of electrical output.

The unit is specified at 8.1 kg and measures 295 × 265 × 190 mm, with a stated mass power density of 370 W/kg. A custom 24 V interface is specified, giving aircraft and equipment developers a basis for electrical and packaging discussions.

A compact generation module helps OEMs assess power demand alongside the mass and packaging requirements of the wider aircraft. Available payload, endurance and total installed mass depend on hydrogen storage, batteries, power electronics and the rest of the platform; the unit rating alone does not establish flight performance.

Bring your propulsion and payload loads, mass budget, altitude and operating conditions to Sydrogen. The team can review whether KZ3000F fits the required power architecture and define the integration and validation scope with your engineering team.