de Havilland Canada DHC-2 Beaver vs. McDonnell Douglas A-4 Skyhawk
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de Havilland Canada DHC-2 Beaver |
versus |
McDonnell Douglas A-4 Skyhawk |
13.56 m |
44 ft 6 in |
length |
12.19 m |
40 ft 0 in |
5 m |
16 ft 5 in |
height |
4.57 m |
15 ft |
16.56 m |
54 ft 4 in |
wingspan |
8.08 m |
26 ft 6 in |
2 x Armstrong Siddeley Double Mamba turboprop engines |
engines |
1x Pratt & Whitney J52-P-6A Jet |
Approximately 3,100 hp (2,312 kW) each |
thrust per engine |
8,500 pound-force |
Approximately 6,200 hp (4,624 kW) total |
total thrust |
8,500 pound-force |
24,200 lb |
10,977 kg |
MTOW |
11,113 kg |
24,500 lb |
2,535 km |
1,369 nm |
range |
3,222 km |
1,739 nm |
228 mph |
367 km/h |
cruise speed |
586 kts |
364 mph |
Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling |
capacity |
Up to 9,155 pounds of weapons on 5 hardpoints |
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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.