Lockheed T-33 Shooting Star vs. McDonnell Douglas F-4 Phantom II

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Lockheed T-33 Shooting Star versus McDonnell Douglas F-4 Phantom II
11.51 m 37 ft 9 in length 19.2 m 63 ft 0 in
3.56 m 11 ft 8 in height 5.03 m 16 ft 6 in
11.9 m 39 ft 1 in wingspan 11.72 m 38 ft 5 in
1 (Allison J33-A-5) engines Two General Electric J79s
24.0 kN thrust per engine 17,900 lbs
24.0 kN total thrust 35,800 lbs
5,900 kg 13,000 lb MTOW 27,965 kg 61,700 lb
2,050 km 1,107 nm range 3,031 km 1,636 nm
965 km/h 600 mph cruise speed Mach 2.2 2,717 km/h
907 kg of bombs or rockets 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.