Lockheed P-2 Neptune vs. Short C-23 Sherpa

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Lockheed P-2 Neptune versus Short C-23 Sherpa
30.17 m 99 ft 0 in length 17.68 m 58 ft 0 in
10.15 m 33 ft 4 in height 6.55 m 21 ft 6 in
33.53 m 110 ft wingspan 22.76 m 74 ft 8 in
2 x Wright R-3350 radial engines engines 2 x Pratt & Whitney Canada PT6A-45R turboprop engines
Approximately 3,700 hp thrust per engine Approximately 1,200 hp per engine
Approximately 7,400 hp total thrust Approximately 2,400 hp total
27,216 kg 60,000 lb MTOW 7,484 kg 16,500 lb
7,885 km 4,259 nm range 1,048 km 566 nm
300 mph 483 km/h cruise speed 425 km/h 264 mph
based on configuration capacity based on configuration
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.