Lockheed U-2 vs. Scottish Aviation T1 Bulldog

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Lockheed U-2 versus Scottish Aviation T1 Bulldog
19.2 m 63 ft 0 in length 7.11 m 23 ft 4 in
4.8 m 15 ft 9 in height 2.08 m 6 ft 10 in
32 m 105 ft wingspan 10.21 m 33 ft 6 in
1 × General Electric F118-101 engines 1 x Lycoming O-360-A4M piston engine
17,000 lbf (76 kN) thrust per engine Approximately 180 hp
17,000 lbf (76 kN) total thrust Approximately 180 hp
18,144 kg 40,000 lb MTOW 1,111 kg 2,450 lb
6,090 nm 11,278 km range 1,050 km 567 nm
475 mph 764 km/h cruise speed 222 km/h 138 mph
capacity Instructor pilot and one student
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.