McDonnell Douglas F-4 Phantom II vs. Tu-144
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McDonnell Douglas F-4 Phantom II |
versus |
Tu-144 |
19.2 m |
63 ft 0 in |
length |
65.7 m |
215 ft 6 in |
5.03 m |
16 ft 6 in |
height |
12.55 m |
41 ft 2 in |
11.72 m |
38 ft 5 in |
wingspan |
28.8 m |
94 ft 6 in |
Two General Electric J79s |
engines |
4 Kolesov RD-36-51 or Kuznetsov NK-144 engines |
17,900 lbs |
thrust per engine |
44,000 pounds (full afterburner) |
35,800 lbs |
total thrust |
176,000 pounds (full afterburner) |
27,965 kg |
61,700 lb |
MTOW |
207,000 kg |
456,300 lb |
3,031 km |
1,636 nm |
range |
3,500 nm |
6,482 km |
Mach 2.2 |
2,717 km/h |
cruise speed |
Mach 2.17 |
2680 km/h |
Up to 16,000 lbs of externally carried ordnance |
capacity |
150 passengers |
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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.