F-4 technical data

Name McDonnell Douglas F-4 Phantom II (data mostly for F-4F)
first flight 27.05.1958 (whole F-4 series) / F-4F 18.03.1973
numbers build (F-4F) 175 / overall 5083
Engines 2 x J79-GE-17A
max. thrust 79,24 kN
empty weight 13757 kg
max. weight 28030 kg
normal T/O weight 18818 kg
max speed low 1464 km/h (Mach 1,19) with 4 Sparrow
max. climb 8534 m/s with J79
max speed high > Mach 2,0
max. altitude > 16500 m
ferry range 3800 km
wing span 11,77 m
wing loading max. 569,2 kN/m2
Length 19,20 m
Wing area 49,2 qm
Height 5,02 m
Take off run 1329 m
Landing run 1152 m (without brakechute) / 951 m (with brakechute)
max. rate of climb at sea level 1881 m/min
rate of climb with 1 engine 1067 m/min
Hardpoints 9