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FotoImages - Aircraft Data McDonnell Douglas A-4 Skyhawk |
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The creation of Douglas chief engineer, Ed Heinemann, the Skyhawk went against the 1950's trend for ever larger combat a/c. Initially weighing less than half the 30,000 lbs stipulated by the US Navy, the A-4 quickly showed is was still capable of carrying out all missions required of it. By Vietnam, the A-4 had become the backbone of the Navy and Marine Corps light attack force and has seen active service extended to current times.
General:
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Type: Fighter |
Crew: 1 |
Seating: 1 |
First Flight: 22/Jun/1954 |
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Specifications |
Propulsion |
Performance |
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Length: Height: Wingspan: Empty Weight: Gross Weight: |
40' 3.25" 15' 0" 27' 6" 10,500 lbs. 27420 lbs. |
No. Engines: Horsepower: Powerplant: |
1
11200
#st per engine
Pratt & Whitney J52-P-408A |
Range (ferry): Speed (max): Speed (cruise): Climb: Ceiling: |
2055 miles 675 mph - mph 5600 ft/sec - ft |
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Armament: |
2x20mm Mk 12 cannon in wing roots, plus a large variety and combination of rockets, bombs & missiles. | ||||
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