F-102 Delta Dagger
| F-102 Delta Dagger |
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| Description |
\n| Role | Interceptor |
\n| Crew | 1 |
| Dimensions |
\n| Length | 68.33 ft | 20.83 m |
\n| Wingspan | 38.08 ft | 11.61 m |
\n| Height | 21.17 ft | 6.45 m |
\n| Wing area | 661.5 sq ft | 61.46 m² |
| Weights |
\n| Empty | 19,050 lb | 8,639 kg |
\n| Loaded | 31,559 lb | 14,314 kg |
\n
| Powerplant |
\n| Engines | One Pratt & Whitney J57 with afterburner |
\n| Power | 16,000 lb | 71 kN |
| Performance |
\n| Maximum speed | 810mph | 1,304 km/h |
\n| Combat range | 1,000 mi | 1609 km |
\n| Ferry range | | |
\n| Service ceiling | 55,000 ft | 16,764 m |
\n| Rate of climb | 12,992 ft/min | 3,960 m/min |
| Armament |
\n| Rockets/Missiles | 24 unguided 2.75 in (70 mm) rockets, six guided missiles |
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The
Convair F-102 Delta Dagger fighter aircraft was part of the backbone of the
United States air defenses in the late
1950s. Entering service in
1956, its main purpose was to
intercept invading
Soviet bomber fleets. However the project was troubled and by the early
1960s the plane was being replaced by F-101 Voodoos and F-4 Phantom IIs. Many of the F-102s were transferred to
United States Air National Guard duty by the mid- to late-1960s, and the plane left service altogether in
1976.
The plane was developed from the XF-92A delta-wing research aircraft of the late
1940s. The Air Force took a new approach in putting out the request for proposals for an operational
interceptor, considering both the aircraft and armament together in what became known as a "weapon system". The RFP for "Project MX-1554" went out
18 June 1950, and in January
1951 six manufacturers responded, of which Convair,
Lockheed, and
Republic were chosen to proceed with design. But three projects were too expensive, and in November, only Convair was allowed to continue with its
Model 8-80, an interim project using the less-powerful Westinghouse J40
turbojet in lieu of the Wright J67 which was still in development.
The
YF-102A made its first flight on
24 October 1953, but was lost in an accident nine days later. The second aircraft flew on
11 January 1954, confirming a dismal performance, far below the requirements. The problem was solved by the use of the area-ruled fuselage, and on
19 December the modified plane,
Model 8-90, first flew, achieving a speed of Mach 1.22 and an altitude of 53,000 ft (16,155 m).
The first operational service of the
F-102A was with the 327th Fighter-Interceptor Squadron at George Air Force Base, in April 1956, and eventually a total of 889 were built. 111
TF-102A two-seat side-by-side trainers were also produced. In
1973 six aircraft were converted to target drones simulating MiG-21s.
The operational Delta Dagger still fell short of its goals, but the planned
F-102B improvements eventually became a new plane, the
F-106 Delta Dart.
Variants
- YF-102A - prototypes\n* F-102A - 889 built\n* TF-102A - two-seat trainer, 111 built\n* QF-102A - two piloted target drones\n* PQM-102A - (at least) four unpiloted target drones
{| cellpadding="2" cellspacing="0" style=";clear:both;margin:5px auto; border:3px solid;width:60%; font-size:small;" align="center"\n!bgcolor="#e0e0e0" colspan="2" align="center" style="border-bottom:3px solid"|Related content\n|-\n|Related Development\n|align="center"|\n|-\n|Similar Aircraft\n|align="center"|\n|-\n|Designation Series\n|align="center"|\nF-99 -\n
F-100 -\n
F-101 -\n
F-102 -\nXF-103 -\n
F-104 -\n
F-105\n|-\n|
Related Lists\n|align="center"|
List of military aircraft of the United States -
List of fighter aircraft\n|-\n|}
Category:US fighter aircraft 1950-1959
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