Boeing 787-10 vs. McDonnell Douglas F-4 Phantom II
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Boeing 787-10 |
versus |
McDonnell Douglas F-4 Phantom II |
68.0 m |
223 ft 2 in |
length |
19.2 m |
63 ft 0 in |
17 m |
55 ft 9 in |
height |
5.03 m |
16 ft 6 in |
60 m |
196 ft 1 |
wingspan |
11.72 m |
38 ft 5 in |
2x Rolls-Royce Trent 1000 or General Electric GEnx-1B |
engines |
Two General Electric J79s |
76,000 N |
thrust per engine |
17,900 lbs |
2 x 76,000 N |
total thrust |
35,800 lbs |
254,000 kg |
560,000 lb |
MTOW |
27,965 kg |
61,700 lb |
11,910 km |
6,430 nmi |
range |
3,031 km |
1,636 nm |
652 mph |
1,050 kph |
cruise speed |
Mach 2.2 |
2,717 km/h |
330 passengers |
capacity |
Up to 16,000 lbs of externally carried ordnance |
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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.