de Havilland Canada DHC-2 Beaver vs. Mitsubishi A6M Zero
... or view the full comparison list
here.
de Havilland Canada DHC-2 Beaver |
versus |
Mitsubishi A6M Zero |
13.56 m |
44 ft 6 in |
length |
9.06 m |
29 ft 9 in |
5 m |
16 ft 5 in |
height |
3.05 m |
10 ft |
16.56 m |
54 ft 4 in |
wingspan |
12 m |
39 ft 4 in |
2 x Armstrong Siddeley Double Mamba turboprop engines |
engines |
1 × Nakajima NK1C Sakae-12 14-cylinder air-cooled radial piston engine |
Approximately 3,100 hp (2,312 kW) each |
thrust per engine |
940 hp for take-off, 950 hp at 4,200 m (13,800 ft) |
Approximately 6,200 hp (4,624 kW) total |
total thrust |
940 hp for take-off, 950 hp at 4,200 m (13,800 ft) |
24,200 lb |
10,977 kg |
MTOW |
2,800 kg |
6,170 lb |
2,535 km |
1,369 nm |
range |
1,010 nm |
1,871 km |
228 mph |
367 km/h |
cruise speed |
180 knots |
105 mph |
Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling |
capacity |
|
|
|
rotor diameter |
|
|
|
|
rate of climb |
|
|
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.