BAC Jet Provost vs. McDonnell Douglas F-4 Phantom II

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BAC Jet Provost versus McDonnell Douglas F-4 Phantom II
10.36 m 34 ft 0 in length 19.2 m 63 ft 0 in
3.1 m 10 ft 2 in height 5.03 m 16 ft 6 in
11.25 m 36 ft 11 in wingspan 11.72 m 38 ft 5 in
1 x Bristol Siddeley Viper 201 engines Two General Electric J79s
2,500 lb = 1,134 kg thrust per engine 17,900 lbs
2,500 lb = 1,134 kg total thrust 35,800 lbs
4,173 kg 9,200 lb MTOW 27,965 kg 61,700 lb
1,448 km 782 nm range 3,031 km 1,636 nm
440 mph 708 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.