Boeing 757-200 vs. McDonnell Douglas F-4 Phantom II
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Boeing 757-200 |
versus |
McDonnell Douglas F-4 Phantom II |
47.3 m |
155 ft 2 in |
length |
19.2 m |
63 ft 0 in |
13.56 m |
44 ft 6 in |
height |
5.03 m |
16 ft 6 in |
38.1 m |
125 ft |
wingspan |
11.72 m |
38 ft 5 in |
Rolls-Royce RB211 or Pratt & Whitney PW2000 |
engines |
Two General Electric J79s |
36,600–43,500 lbf (163–193 kN) |
thrust per engine |
17,900 lbs |
77,000 to 80,000 pounds |
total thrust |
35,800 lbs |
115,666 kg |
255,000 lb |
MTOW |
27,965 kg |
61,700 lb |
6,300 km |
3,400 nm |
range |
3,031 km |
1,636 nm |
876 km/h |
544 mph |
cruise speed |
Mach 2.2 |
2,717 km/h |
200 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.