Airbus A220-300 vs. Lockheed T-33 Shooting Star

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Airbus A220-300 versus Lockheed T-33 Shooting Star
38.7 m 127 ft 0 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 x Pratt & Whitney PurePower PW1500G 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
70,900 kg 156,300 lb MTOW 5,900 kg 13,000 lb
6,297 km 3,402 nm range 2,050 km 1,107 nm
Mach 0.82 101,3 km/h cruise speed 965 km/h 600 mph
Typical seating 2-class 120-150 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.