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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