North American B-25 Mitchell vs. Percival Provost

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North American B-25 Mitchell versus Percival Provost
16.15 m 53 ft 0 in length 9.0 m 29 ft 6 in
5 m 16 ft 4 in height 3.02 m 9 ft 11 in
20.58 m 67 ft 6 in wingspan 12.19 m 40 ft
2 x Wright R-2600-92 Twin Cyclone engines 1 x Alvis Leonides Major 755/1 inline engine
1,700 horsepower thrust per engine Approximately 550 hp
3,400 horsepower total thrust Approximately 550 hp
7,484 kg 16,500 lb MTOW 5,500 lb 2,495 kg
1,350 mi 1,175 nm range 1,127 km 608 nm
233 MPH 375 km/h cruise speed 175 mph 282 km/h
capacity Pilot and one passenger
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.