Boeing 777-200 vs. McDonnell Douglas F-4 Phantom II
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Boeing 777-200 |
versus |
McDonnell Douglas F-4 Phantom II |
63.7 m |
209 ft 1 in |
length |
19.2 m |
63 ft 0 in |
18.6 m |
61 ft |
height |
5.03 m |
16 ft 6 in |
64.8 m |
212 ft 7 in |
wingspan |
11.72 m |
38 ft 5 in |
General Electric GE90-77B or GE90-94B, Pratt & Whitney PW4077 & PW4090, Rolls-Royce Trent 877 & Trent 895 |
engines |
Two General Electric J79s |
Up to 94,000 pounds |
thrust per engine |
17,900 lbs |
Up to 188,000 pounds |
total thrust |
35,800 lbs |
299,370 kg |
660,000 lb |
MTOW |
27,965 kg |
61,700 lb |
5,240 nm |
9,711 km |
range |
3,031 km |
1,636 nm |
560 mph |
901 km/h |
cruise speed |
Mach 2.2 |
2,717 km/h |
305 |
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.