Airbus A220-100 vs. Folland Gnat

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Airbus A220-100 versus Folland Gnat
35.0 m 114 ft 10 in length 9.67 m 31 ft 9 in
11.5 m 37 ft 9 in height 2.95 m 9 ft 8 in
35.1 m 115 ft 2 in wingspan 7.32 m 24 ft
2 Turbofans (wing mounted) engines Bristol Siddeley Orpheus 100
21,000–23,000 lb thrust per engine 4700 lbf
42,000–46,000 lb total thrust 4700 lbf
63,100 kg 139,100 lb MTOW 3,915 kg 8,630 lb
6,390 km 3,451 nm range 1,851 km 999 nm
871 km/h 541 mph cruise speed 360 mph 579 km/h
Typical seating 2-class 100-120 capacity Single or two-seat light fighter and trainer aircraft
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.