Commonwealth CA-25 Winjeel vs. Lockheed U-2

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Commonwealth CA-25 Winjeel versus Lockheed U-2
7.77 m 25 ft 6 in length 19.2 m 63 ft 0 in
2.84 m 9 ft 4 in height 4.8 m 15 ft 9 in
10.82 m 35 ft 6 in wingspan 32 m 105 ft
1 x Pratt & Whitney R-985-AN-2 radial engine engines 1 × General Electric F118-101
Approximately 450 hp thrust per engine 17,000 lbf (76 kN)
Approximately 450 hp total thrust 17,000 lbf (76 kN)
5,650 lb 2,563 kg MTOW 18,144 kg 40,000 lb
1,287 km 695 nm range 6,090 nm 11,278 km
150 mph 241 km/h cruise speed 475 mph 764 km/h
Instructor pilot and one student 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.