Tupolev TU-155 vs. McDonnell Douglas F-4 Phantom II

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Tupolev TU-155 versus McDonnell Douglas F-4 Phantom II
47.63 m 156 ft 3 in length 19.2 m 63 ft 0 in
16.4 m 53 ft 10 in height 5.03 m 16 ft 6 in
64.9 m 212 ft 11 in wingspan 11.72 m 38 ft 5 in
4 × Kuznetsov NK-321 turbofans engines Two General Electric J79s
304.5 kN (68,500 lbf) thrust per engine 17,900 lbs
1,218 kN (274,000 lbf) total thrust 35,800 lbs
640,000 kg 1,411,000 lb MTOW 27,965 kg 61,700 lb
7,000 km 3,780 nm range 3,031 km 1,636 nm
850 km/h 528 mph cruise speed Mach 2.2 2,717 km/h
350 passengers capacity Up to 16,000 lbs of externally carried ordnance
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.