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The Convair F-102 Delta Dagger resulted from a 1950 USAF design competition for an integral all-weather interceptor weapon system. Combining the Hughes Falcon air-to-air missile, the delta wing platform first flown on the XF-92A, and the 4944kg thrust Pratt & Whitney J57-P-11 turbojet, the first of 10 YF-102s (52-7994/7995 and 53-1779/1786) flew at Edwards AFB, California, on 24 October 1953. The prototype was lost in a mishap nine days later, but tests with other YF-102 airframes revealed a disappointing truth: the type was sorely underpowered and incapable of level supersonic flight. Rarely had the Air Force invested so much in a system which performed so poorly.
Convair designers went back to the drawing board and the indented fuselage or 'area rule' configuration developed by NACA's Richard Whitcomb was hastily introduced in the much-altered YF-102A, which was assembled in a scant 117 days. The first of four YF-102As (53-1787/1790) flew at Edwards AFB on 20 December 1954, not merely with 'area rule' but with cambered wing, new canopy (except on 53-1788) and 5443kg thrust Pratt & Whitney J57-P-23. The new design was supersonic and met USAF expectations.
The production F-102A began to reach Air Defense Command squadrons in June 1955. The first two-seat TF-102A combat proficiency trainer (54-1351) flew at Edwards AFB 8 November 1955 and operated alongside F-102As in ADC service. Total Delta Dagger production was 873 airplanes.
The F-102B designation was briefly assigned to a new aircraft completed as the F-106. The little-known YF-102C (53-1806), a converted F-102A model, tested change in the internal fire control system, but these were not adopted.
A rakish, well-liked and easily-handling aircraft, popular out of proportion to its importance, the F-102A eventually served with 27 ADC and 23 ANG squadrons. Air Defense Command machines went through several modernisation programmes before being relegated to the ANG, the internal provision for rockets being eventually omitted. A few F-102As went to Greece and Turkey. A few camouflaged F-102As were deployed to South East Asia in 1964-6, and to trouble-plagued Korea in 1968 but, while they flew a few missions over North Vietnam, they are not thought to have actually been in combat.
The PQM-102A is a Sperry-converted airframe under the Pave Deuce programme for use as a fully manoeuvrable manned or unmanned target drone. About 30 have been converted. Numerous F-102A airframes have been saved, the 199th Fighter Interceptor Squadron of the Hawaii Air National Guard having retained no fewer than four non-flyable F-102As for display purposes after transitioning to the F-4C Phantom.
 | A three-view drawing (1680 x 1223) |
| CREW | 1 |
| ENGINE | 1 x turbo-jet P+W J-75-P-17(N), 107.0kN |
| WEIGHTS |
| Take-off weight | 15900 kg | 35054 lb |
| Empty weight | 10730 kg | 23656 lb |
| DIMENSIONS |
| Wingspan | 11.7 m | 38 ft 5 in |
| Length | 21.6 m | 70 ft 10 in |
| Height | 6.2 m | 20 ft 4 in |
| Wing area | 64.8 m2 | 697.50 sq ft |
| PERFORMANCE |
| Max. speed | 2300 km/h | 1429 mph |
| Cruise speed | 2010 km/h | 1249 mph |
| Ceiling | 16000 m | 52500 ft |
| Range w/max.fuel | 2400 km | 1491 miles |
| Jeff, CarGuyOne(@)aol.com, 16.07.2008 The Air National Guard had these at Ellington AFB, TX, in the 1960s before they upgraded. Lt. George W Bush flew 102s with this unit. | | Max Kohnke, maxsmodels(@)yahoo.com, 28.06.2008 I have seen several references to a F-102 being shot down by a MiG in Viet Nam on an escort mission for B-52s. There was a great deal of judgemental error by the brass in using a dedicated interecptor, optimized for radar intercepts against bombers as an escort fighter over enemy territory in clear weather. Virtually all of the F-102's advantages (all weather radar, speed & altitude) were lost while it's weaknesses (no guns or no rearward visibility) were exploited by the enemy. | | Roger Moore, RV4DRVR(@)aol.com, 14.06.2008 I flew the 102 for both the Hawaii and Conn. Ang from 1965 to 1968 and it was a delight to fly. I then flew the F100 for the DC ANG briefly in 1970 and in the pattern they felt the same but the 102 was vastly superior in ceiling and turn rate. The USAF offered me a 90 day tour in Vietnam in 1966 but I declined as the 102 was no rival for the MIG 21. | | Butch Owens, butch130j(@)yahoo.com, 09.05.2008 I was a crew chief on the F-102A at Clark AFB, Phillipines, Tan Son Nhut AFB in Saigon, Vietnam and at Udorn and Don Muong, Thailand in 1965 and 1966. Also worked Dueces in the 51st OMS (16th) FIS at Naha AFB, Okinawa in 1961 and 1962. The Duece was a challenging aircraft but was loved by maintainers and pilots as well. | | Mel, flyboymel(@)sbcglobal.net, 30.04.2008 You have the F-106 spec's instead of the F-102 spec's. |
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|  COMPANY PROFILE
FACTS AND FIGURES© To make it supersonic, the
original YF-102 was
lengthened and given bulges
on the rear fuselage to
change the cross-section.
These protuberances were
known as 'Marilyns'. © The YF-102 was a
development of the XF-92
research aircraft, which was
originally to be the ramjet-powered
'return' component
of a large two-part composite
attack aircraft. © The canopy of the YF-102
had heavy framing more
akin to an early World War
II fighter. Convair were
probably worried about the
stress of supersonic flight on
large areas of Perspex.
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