Specifications
Country of Origin: United States
Manufacturer: Convair Division of General Dynamics
Role/Function: Fighter-Interceptor
Serial Number: 58-0793 (Displayed as 57-2456).
Model Number/Mk. #: Model 8-24
Crew: 1
Power Plant: 1 - Pratt & Whitney J75-P-17 Turbojet engine, 24,500 lbs. thrust in afterburner.
Maximum Speed: 1,525 mph (Mach 2.3) @ 40,000 ft.
Cruising Speed: n/a
Service Ceiling: 53,000 ft.
Range: 1,500 miles (Combat radius - 730 miles).
Weights: Empty: 23,650 lbs. Gross: 38,700 lbs.
Wing Span: 38 ft. 3½ in.
Length: 70 ft. 9 in. (including pitot tube).
Height: 20 ft. 3 in.
Wing Area: 661.5ft²/61.52m² (Original Wing) or 695 ft²/64.57m² (Conically-Cambered Wing)
Armament: 1 - AIR-2A Genie nuclear tipped rocket and 4 - AIM-4 Falcon missiles in internal weapons bay. (AIR-2A replaced by the M61A1 Vulcan 20mm cannon in some aircraft,)
Cost: $4,700,000.00
# Built: n/a
# in Current Service: Starting in 1986, many of the surviving aircraft were converted into drones, designated QF-106A, and used for target practice. The last was destroyed in January 1998. The drones were still capable of being flown as manned aircraft, such as for ferrying to a test; during the test they were flown unmanned. A handful of F-106s were retained by NASA for test purposes through 1998.