Airbus A220-100 vs. Lockheed SR-71 Blackbird

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Airbus A220-100 versus Lockheed SR-71 Blackbird
35.0 m 114 ft 10 in length 32.74 m 107 ft 5 in
11.5 m 37 ft 9 in height 5.64 m 18 ft 6 in
35.1 m 115 ft 2 in wingspan 16.94 m 55 ft 7 in
2 Turbofans (wing mounted) engines Two Pratt & Whitney J58 axial-flow turbojets
21,000–23,000 lb thrust per engine 34,000 lbs
42,000–46,000 lb total thrust 68,000 lbs
63,100 kg 139,100 lb MTOW 78,018 kg 172,000 lb
6,390 km 3,451 nm range 3,250 mi 2,832 nm
871 km/h 541 mph cruise speed Mach 3.2 3951 km/h
Typical seating 2-class 100-120 capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.