Photos from the personal collection of Konstantinos Panitsidis
Technical specifications 
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THREE-VIEW DRAWING
TECHNICAL SPECIFICATIONS
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DESIGNER
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McDonnell Douglas
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COUNTRY
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USA
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TYPE
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Multipurpose fighter
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CREW
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2
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POWER-PLANT
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Two General Electric J79-GE-17C
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Thrust, kN
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2 x 81,40
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DIMENSIONS
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Length, m
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19,20
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Height, m
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5,03
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Wing span, m
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11,71
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Wing area m2
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49,24
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WEIGHT
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Empty aircraft, kg
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13.397
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| Normal take-off, kg |
-
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| Maximum take-off, kg |
17.964
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Useful load, kg
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-
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PERFORMANCE
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Maximum speed, km/h
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2.410
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Max speed in low height, km/h
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-
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| Ferry range, km | - |
| Range, km |
4.180
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| Combat range, km |
958
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| Rate of climb, m/min |
15.200
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Service ceiling, m
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21.600
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Maximum overload, g
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- |
| ARMAMENT | 1x 20 mm cannon M61A1. Warload - 7.258 kg in 9 hardpoints. Possibility of transport: 4-6 Air-to-air missile AIM-7E/F/M Sparrow or Skyflash, 4x AIM-9 Sidewinder or up to 6 Air-to-surface missile AGM-65 Maverick. Bombs GBU-16 Paveway II, AGM-145A/B JSOW, Paveway II/III. Bombs Mk.82, B117 or BLU-10/B. 1x 20 kT nuclear bomb B57 or 100/500 kT B61. 4 pods GBU-4 with 30 mm cannon GAU-13A and 300 rounds or 4 pods SUU-16A or -23A with 20-cannon M61A1 or GAU-4 and 1.200 rounds 5 external tank (5 x 1.401 ltr). |
PHOTOS F-4E Peace Icarus 2000
