Aermacchi MB-326 vs. McDonnell Douglas F-4 Phantom II

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Aermacchi MB-326 versus McDonnell Douglas F-4 Phantom II
10.67 m 35 ft 0 in length 19.2 m 63 ft 0 in
3.71 m 12 ft 2 in height 5.03 m 16 ft 6 in
10.82 m 35 ft 6 in wingspan 11.72 m 38 ft 5 in
1 x Rolls-Royce “Viper” 632-42 turbojet engines Two General Electric J79s
4,000 lb thrust per engine 17,900 lbs
4,000 lb total thrust 35,800 lbs
5,897 kg 13,000 lb MTOW 27,965 kg 61,700 lb
677 mi 589 nm range 3,031 km 1,636 nm
553 mph 890 km/h cruise speed Mach 2.2 2,717 km/h
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.