The Convair F-102 A 'Delta Dagger', commonly referred to as the 'Deuce', was the USAF's first operational supersonic interceptor and delta wing fighter. They were part of the Air Defense Command (ADC) which in turn was part of the North American Aerospace Defense Command (NORAD). A total of 889 F-102 A's were produced and they were in service between 1956 and 1979. F-102 A's were used in Southeast Asia as early as 1962. While I was serving in Southeast Asia in 1966 and 1967, F-102 A's of the 64th and 509th Fighter Interceptor Squadrons (FIS) of the 405th Fighter Wing (FW), 13th Air Force, PCAF. were used on a rotational basis in Bien Hoa AB and Da Nang AB, Vietnam, and Udorn RTAB, and Don Muang AB, Thailand. F-102s were also used by Turkey and Greece. In Southeast Asia besides functioning as interceptors, they were primarily used for combat air patron (CAP) missions for B-52's and for air ground support using their 24 2.75 in (70 mm) rockets. Specifications for F-102 A Crew: 1 Length: 68-ft 4-in (20.83 m) Wingspan: 38-ft 1-in (11. 61 m) Height: 21-ft 2-in (6.45 m) Wing area: 661.5 sq ft/ 61.52 sq m (Original Wing) or 695 sq ft / 64.57 sq m (Conically-Cambered Wing) Empty weight: 19,350 lb (8,777 kg) Loaded Weight: 24,500 lb (11,100 kg) Max. takeoff weight: 31,500 lb (14,300 kg) Powerplant: 1 x Pratt & Whitney J57-P-25 afterburning turbojet Dry thrust: 11,700 lbf Thrust with afterburner: 17,200 lbf Performance: Maximum speed: Mach 1.25 (825 mph, 1,304 km/h) at 40,000 ft (12,190 m) Range: 1,350 mi (1,170 nmi, 2,175 kn) Service ceiling: 53,400 ft (16, 300 m) Rate of climb: 13,000 ft/min Thrust/wight: 0.70 Armament Rockets: 24 x 2.75 (70 mm) FFAR (Folding Fin Aerial Rocket) unguided rockets in missile bay doors Missiless: 6 x AIM-4 Falcon air-to-air missiles or 3 x AIM-4 Falcon 1 x AIM-26 Falcon with conventional or nuclear warhead Avionics MG-10 fire control system This picture was taken at Pima Air Museum, Tucson on 29 October 2016, Sig...