Airbus A220-100 vs. Lockheed T-33 Shooting Star

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Airbus A220-100 versus Lockheed T-33 Shooting Star
35.0 m 114 ft 10 in length 11.51 m 37 ft 9 in
11.5 m 37 ft 9 in height 3.56 m 11 ft 8 in
35.1 m 115 ft 2 in wingspan 11.9 m 39 ft 1 in
2 Turbofans (wing mounted) engines 1 (Allison J33-A-5)
21,000–23,000 lb thrust per engine 24.0 kN
42,000–46,000 lb total thrust 24.0 kN
63,100 kg 139,100 lb MTOW 5,900 kg 13,000 lb
6,390 km 3,451 nm range 2,050 km 1,107 nm
871 km/h 541 mph cruise speed 965 km/h 600 mph
Typical seating 2-class 100-120 capacity 907 kg of bombs or rockets
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.