Lockheed P-2 Neptune vs. Beechcraft King Air 260
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Lockheed P-2 Neptune |
versus |
Beechcraft King Air 260 |
30.17 m |
99 ft 0 in |
length |
13.41 m |
43 ft 11 in |
10.15 m |
33 ft 4 in |
height |
4.57 m |
15 ft |
33.53 m |
110 ft |
wingspan |
17.39 m |
57 ft 1 in |
2 x Wright R-3350 radial engines |
engines |
2 x Pratt & Whitney Canada PT6A turboprop |
Approximately 3,700 hp |
thrust per engine |
1050 lbs |
Approximately 7,400 hp |
total thrust |
2100 lbs |
27,216 kg |
60,000 lb |
MTOW |
12,500 lb |
5,670 kg |
7,885 km |
4,259 nm |
range |
1,720 nm |
3,185 km |
300 mph |
483 km/h |
cruise speed |
310 kts |
193 mph |
based on configuration |
capacity |
9 |
|
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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.