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