Convair F-102A Delta Dagger (8-10) Aircraft Data
All-weather, day/night, sonic interceptor. The F-102A is a single-engine, delta wing design, relying on rocket and missile armament to intercept and dispatch enemy bombers. Active with the United States Air Force (USAF) from 1956-1970, the F-102 saw combat in Vietnam as a forward air-controller. In addition to the 889 single-seat F-102A's which were built, 111 two-seat TF-102A's were also built by Convair. Turkish F-102A's were used against Greek forces during the invasion of Cyprus, the former alleging a victory over a Greek F-5A.
- Country of Origin: United States
- First Flight: 10/24/53
- Initial Service Date: 4/1/56
- No. Built: 889
- No. In Service: 0
- No. of Hardpoints: 2
- Crew: 1
Power:
1 Pratt & Whitney J57-P-25 afterburning turbojet at 17,200 lbf
Weapons:
24 x 2.75 in. Folding-Fin Aerial Rockets (FFAR), mounted in the bay doors with 6 x AIM-4 'Falcon' air-to-air missiles (AAM). The F-102A carried all weapons in two internal storage bays. No gun armament was ever fitted to any F-102A during operational service. An alternative arrangement had 3 of the AIM-4's replaced by a single AIM-26 nuclear AAM.
Dimensions:
Length: | 68 ft. 4 in. |
Wing Span: | 38 ft. 1 in. |
Wing Area: | 695 sq.ft |
Height: | 21 ft. 2 in. |
Empty Weight: | 19,350 lbs |
Max. Weight: | 31,500 lbs |
Max. Ordnance Load: | 1,250 lbs |
Max. Payload: | 12,150 lbs |
Internal Fuel: | 9,054.76 lbs |
Performance:
Max. Speed: | 825 mph |
Cruise Speed: | 600 mph |
Service Ceiling: | 55,000 ft. |
Normal Range: | 1,350 nm |