Lockheed P-2 Neptune vs. Bell 206
... or view the full comparison list
here.
Lockheed P-2 Neptune |
versus |
Bell 206 |
30.17 m |
99 ft 0 in |
length |
12.11 m |
39 ft 9 in |
10.15 m |
33 ft 4 in |
height |
2.88 m |
9 ft 5 in |
33.53 m |
110 ft |
wingspan |
|
|
2 x Wright R-3350 radial engines |
engines |
1 × Allison 250-C20B |
Approximately 3,700 hp |
thrust per engine |
420 shp (313 kW) |
Approximately 7,400 hp |
total thrust |
420 shp (313 kW) |
27,216 kg |
60,000 lb |
MTOW |
1,451 kg |
3,199 lb |
7,885 km |
4,259 nm |
range |
374 km |
202 nm |
300 mph |
483 km/h |
cruise speed |
222 km/h |
138 mph |
based on configuration |
capacity |
1 pilot + 4 passengers |
|
|
rotor diameter |
11.00 m |
36 ft 1 in |
|
|
rate of climb |
425 m/min |
1,395 ft/min |
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.