Cessna A-37 Dragonfly vs. de Havilland Canada DHC-2 Beaver

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Cessna A-37 Dragonfly versus de Havilland Canada DHC-2 Beaver
8.617 m 28 ft 3 in length 13.56 m 44 ft 6 in
2.71 m 8 ft 11 in height 5 m 16 ft 5 in
10.94 m 35 ft 11 in wingspan 16.56 m 54 ft 4 in
2 x General Electric J85-GE-17A turbojets engines 2 x Armstrong Siddeley Double Mamba turboprop engines
2,850 lbs thrust per engine Approximately 3,100 hp (2,312 kW) each
2 x 2,850 lbs = 5,700 lbs total thrust Approximately 6,200 hp (4,624 kW) total
6,350 kg 14,000 lb MTOW 24,200 lb 10,977 kg
460 nmi 852 km range 2,535 km 1,369 nm
489 mph 787 km/h cruise speed 228 mph 367 km/h
3,000 pounds of bombs, rockets and missiles capacity Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.