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 |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.