Lockheed P-2 Neptune vs. Nanchang CJ-6
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Lockheed P-2 Neptune |
versus |
Nanchang CJ-6 |
30.17 m |
99 ft 0 in |
length |
8.48 m |
27 ft 10 in |
10.15 m |
33 ft 4 in |
height |
2.67 m |
8 ft 9 in |
33.53 m |
110 ft |
wingspan |
10.49 m |
34 ft 5 in |
2 x Wright R-3350 radial engines |
engines |
1 x Ivchenko AI-14RA radial engine |
Approximately 3,700 hp |
thrust per engine |
Approximately 260 hp |
Approximately 7,400 hp |
total thrust |
Approximately 260 hp |
27,216 kg |
60,000 lb |
MTOW |
3,858 lb |
1,751 kg |
7,885 km |
4,259 nm |
range |
800 km |
432 nm |
300 mph |
483 km/h |
cruise speed |
155 mph |
249 km/h |
based on configuration |
capacity |
Pilot and one passenger |
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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.