Hydrogen-Driven Range-Extended Aircraft

(being planned)
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General specifications

  • Wingspan: 20 m
  • Maximum take-off mass: 2t
  • Empty mass: 1t
  • Payload capacity: 1t
  • Loading and unloading < 20 min.
  • Mission change: logistics to firefighting… < 3h
  • Take-Off Distance: < 250 m
  • Propulsion: 2 electric motors, 475 kW each
  • REX: H2/E-Fuel direct combustion system

Flight performance data

  • Short take-off and landing distances
  • Grass/Field Runway Capable
  • Cruising speed: 170 knots (300 km/h)
  • Range: 900–2.000 km

Possible applications

  • Commercial: logistics, supply, telecommunications, surveillance …
  • Disaster control: fire-fighting, supply, surveillance, rescue …
  • Military use: supply, surveillance, telecommunications, rescue …

Technical components

  • E-Axial motors
  • SafeBatt2Fly battery storage
  • SiC power electronics
  • H2L hydrogen energy storage
  • H2-REX

Some components are now in flight testing, at TR level 7-8.

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