Attribute | North American B-25 Mitchell × | Northrop Grumman E-2C Hawkeye 2000 × |
---|---|---|
General | ||
Manufacturer | North American Aviation NAA | Northrop Grumman |
Model | North American B-25 Mitchell | Northrop Grumman E-2C Hawkeye 2000 |
Country | United States | United States |
Manufactured from (year) | 1940 | 1988 |
Manufactured to (year) | 1945 | - |
Type | Military Propellor Planes | Military Propellor Planes |
Icao | B25 | E2 |
Performance | ||
Engine | 2x Wright R-2600-92 Twin Cyclone | 2x 2 X Rolls-Royce T56-A-427 turboprops |
Power, hp (hp) | 1,700 | 5,100 |
Avionics | - | Advanced Control Indicator Set |
1↑Max cruise speed (km/h) | 437 | 648 |
Approach speed (km/h) | 148 | 191 |
Travel range (km) | 2,167 | 2,856 |
Fuel economy (km/l) | - | 1.864 |
Service ceiling (m) | 7,376 | 11,278 |
Rate of climb (m/sec) | 5.08 | 12.78 |
Take off distance (m) | - | 793 |
Landing distance (m) | - | 439 |
Weights | ||
Max take off weight (kg) | 15,876 | 26,082 |
Max payload (kg) | 3,060 | 1,800 |
Fuel tank capacity (l) | 3,687 | 7,003 |
Dimensions | ||
Seats | 5 | 5 |
Exterior length (m) | 16.13 | 17.56 |
Tail height (m) | 4.98 | 5.58 |
Fuselage diameter (m) | 1.4 | 1.9 |
Wing span (m) | 20.6 | 24.56 |
Wing tips | No Winglets | No Winglets |