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APUS i-2

Wing
  • Area: 18m²
  • Span: 12.6m
  • Aspect Ratio: 8.82
Fuselage
  • Length: 8.5m
  • Height: 3.3m
  • Width: 1.4m
Horizontal Stabiliser
  • Gross Area: 3.4m²
  • Span: 3.9m
Masses
  • MTOM: 1,800kg
  • Empty Weight: 1,300kg
  • Payload: 500kg
  • Crew: 1
  • Pax: 3
Performance
  • Max. Endurance (at 50% PWR): 5.2h
  • Max. Range (at 75% PWR): 550 NM
  • Max. Cruise Speed (at 100% PWR at 8,500 ft): 150 KTAS
  • Max. Hydrogen Mass / Tank Capacity: 22kg
  • Max. Gravimetric Energy Density (system based): 2.0 kWh/kg
    (max. achieved in cars 1.6 kWh/kg, batteries 0.3 kWh/kg)

APUS i-2 is the first emission-free aircraft for daily use. It is a four-seat Normal-Category (CS-23) aircraft with 1,800 kg MTOM, a range of 800 km and a maximum cruise speed of 150 KTAS – competitive performance data comparable to most modern four-seat aircraft. Employing a hydrogen fuel-cell as its primary source of energy makes APUS i-2 100% emission-free, i.e. zero CO2, zero NOx, zero noise – nothing less than a revolution in emission-free flying. This is achieved through APUS’s patented structurally integrated hydrogen storage system, known as TubeStruct™. It permits up to 25% higher specific energy density vs. standard hydrogen fuel tanks and 10X better energy density than fully-electric aircraft, all while avoiding the use of rare minerals that batteries do.

Key-Facts:

  • 100% emission-free
  • Competitive range, speed, endurance and payload