de Havilland Canada DHC-2 Beaver vs. Lockheed T-33 Shooting Star

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de Havilland Canada DHC-2 Beaver versus Lockheed T-33 Shooting Star
13.56 m 44 ft 6 in length 11.51 m 37 ft 9 in
5 m 16 ft 5 in height 3.56 m 11 ft 8 in
16.56 m 54 ft 4 in wingspan 11.9 m 39 ft 1 in
2 x Armstrong Siddeley Double Mamba turboprop engines engines 1 (Allison J33-A-5)
Approximately 3,100 hp (2,312 kW) each thrust per engine 24.0 kN
Approximately 6,200 hp (4,624 kW) total total thrust 24.0 kN
24,200 lb 10,977 kg MTOW 5,900 kg 13,000 lb
2,535 km 1,369 nm range 2,050 km 1,107 nm
228 mph 367 km/h cruise speed 965 km/h 600 mph
Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling capacity 907 kg of bombs or rockets
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.