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The A-7 Corsair II was initially developed in response to a 1963 U.S. Navy requirement for an aircraft to replace the Douglas A-4 Skyhawk. Since the Navy wanted the aircraft to be in service by 1967 speed of development was essential. The Vought company based their contract winning design on their F-8 Crusader which was already in Navy service. The prototype flew in 1965 and the first A-7 squadron entered combat in Vietnam in December 1967. The plane proved to be wildly successful as a close air support and strike aircraft. In 1968, the A-7D version of the Corsair II went into production. At the same time production began of the A-7E version for the Navy. These last two versions of the Corsair II are basically identical with the main difference being the equipment installed in the "E" for carrier operations.
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| Wingspan |
36 ft 4 in |
| Length |
13 ft 11 in |
| Weight |
26,000 lbs (loaded) |
| Maximum Speed |
715 mph |
| Service Ceiling |
45,000 ft |
| Range |
2,700 miles |
| Engines |
1 Allison TF41-A-1 turbofan, 14,500 lbs thrust |
| Crew |
1 |
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