McDonnell Douglas F-4 Phantom II vs. North American B-25 Mitchell
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McDonnell Douglas F-4 Phantom II |
versus |
North American B-25 Mitchell |
19.2 m |
63 ft 0 in |
length |
16.15 m |
53 ft 0 in |
5.03 m |
16 ft 6 in |
height |
5 m |
16 ft 4 in |
11.72 m |
38 ft 5 in |
wingspan |
20.58 m |
67 ft 6 in |
Two General Electric J79s |
engines |
2 x Wright R-2600-92 Twin Cyclone |
17,900 lbs |
thrust per engine |
1,700 horsepower |
35,800 lbs |
total thrust |
3,400 horsepower |
27,965 kg |
61,700 lb |
MTOW |
7,484 kg |
16,500 lb |
3,031 km |
1,636 nm |
range |
1,350 mi |
1,175 nm |
Mach 2.2 |
2,717 km/h |
cruise speed |
233 MPH |
375 km/h |
Up to 16,000 lbs of externally carried ordnance |
capacity |
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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.