Mit dem Laden des Videos akzeptieren Sie die Datenschutzerklärung von YouTube.
Mehr erfahren
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