Lockheed P-2 Neptune vs. Percival Provost

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Lockheed P-2 Neptune versus Percival Provost
30.17 m 99 ft 0 in length 9.0 m 29 ft 6 in
10.15 m 33 ft 4 in height 3.02 m 9 ft 11 in
33.53 m 110 ft wingspan 12.19 m 40 ft
2 x Wright R-3350 radial engines engines 1 x Alvis Leonides Major 755/1 inline engine
Approximately 3,700 hp thrust per engine Approximately 550 hp
Approximately 7,400 hp total thrust Approximately 550 hp
27,216 kg 60,000 lb MTOW 5,500 lb 2,495 kg
7,885 km 4,259 nm range 1,127 km 608 nm
300 mph 483 km/h cruise speed 175 mph 282 km/h
based on configuration 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.