Comparison of North American B-25 Mitchell and Northrop Grumman E-2C Hawkeye 2000

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
Max cruise speed (km/h)	437	648
Approach speed (km/h)	148	191
^1↑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