Boeing 737-900ER vs. McDonnell Douglas F-4 Phantom II

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Boeing 737-900ER versus McDonnell Douglas F-4 Phantom II
42.1 m 138 ft 2 in length 19.2 m 63 ft 0 in
12.57 m 41 ft 3 in height 5.03 m 16 ft 6 in
35.8 m 117 ft 5 in wingspan 11.72 m 38 ft 5 in
2x CFM56-7B24/26/27 Turbofan engines Two General Electric J79s
28,400 pound-force thrust per engine 17,900 lbs
56,800 pound-force total thrust 35,800 lbs
85,139 kg 187,800 lb MTOW 27,965 kg 61,700 lb
3,235 nm 5,990 km range 3,031 km 1,636 nm
510 knots 296 mph cruise speed Mach 2.2 2,717 km/h
178 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.