Designed to replace the F-84, the Republic F-105 Thunderchief was unquestionably one of the finest fighter-bombers of all time and probably the most important tactical strike aircraft of the USAF during the Vietnam War. Designed by Alexander Kartveli and known affectionately as the "Thud", the F-105 was capable of deliviering up 6,700 different combinations of weapons (both conventional and nuclear) which included every US tactical missile and bomb during its time. It was also a large aircraft: the largest single-engined fighter ever used by the USAF but it could deliver a greater payload than a World War II-era heavy bomber, far more accurately, and doing it at supersonic speeds. The F-105 ultimately became Tactical Air Command's foremost strike aircraft during the 1960s, notably during the Rolling Thunder bombing campaign against North Vietnam: a total of over 380 F-105s were lost in combat, a testament to the intensity of their operations. Thunderchiefs were also used as Wild Weasel anti-radar operations but were slowly phased out in most roles by the F-4. There were no exports of this outstanding aircraft and were finally retired from reserve units in 1984.
The first YF-105A prototype had its maiden flight on 22 October 1955 and was ordered into production as the F-105B as well as the RF-105B photo-reconnaissance platform. Next up was the F-105D which featured new enignes, strengthened structures, a new search and ranging radar, and all-weather capability via an integrated fire control system. Later, the F-105F was intended as a combat capable trainer but many were converted to EF-105F Wild Weasel anti-radar platforms followed by the similar F-105G with new avionics.
Preceded by:
F-84 Thunderjet (1947)Succeeded by:
F-111 Aardvark (1967)Design | F-105B | F-105D | F-105G |
Name | Thunderchief | Thunderchief | Wild Weasel |
Type | Fighter-Bomber | Fighter-Bomber | Electronic Attack |
Year | 1958 | 1961 | 1967 |
Crew | 1 | 1 | 2 |
Dimensions | |||
Length | 19.23 m | 19.63 m | 20.42 m |
Height | 5.994 m | 5.994 m | 6.147 m |
Wing Span | 10.65 m | 10.65 m | 10.65 m |
Wing Area | n/a | n/a | n/a |
Weight | |||
Empty | 11,728 kg | 12,474 kg | 12,474 kg |
Loaded | 16,165 kg | 18,177 kg | |
Maximum | 23,587 kg | 23,835 kg | 24,506 kg |
Wing Loading | 659.5 kg/m² | 666.4 kg/m² | 685.2 kg/m² |
Performance | |||
Speed | Mach 2.1 | Mach 2.2 | Mach 2.1 |
Speed S/L | ? | Mach 1.1 | Mach 1.2 |
Cruise Speed | ? | ? | 959 km/h |
Ceiling | 15,240 m | 15,240 m | 15,240 m |
Range | 3,589 km | 1,252-3,556 km | 1,191-2,414 km |
Powerplant | |||
Engine | 1 x J75-P-19 Pratt & Whitney 7,471 / 11,113 (+) kgf | 1 x J75-P-19W Pratt & Whitney 7,802 / 12,020 (+) kgf | 1 x J75-P-19W Pratt & Whitney 7,802 / 12,020 (+) kgf |
Fuel Load | n/a | 3,557 kg | 3,223 kg |
Thrust/Weight | 0.58 | 0.57 | 0.57 |
Sensors | |||
Radar | AN/APN-105 | AN/APN-131 | AN/APN-196 |
Armament | |||
Guns | 1 x 20-mmM61A1 (1,028) | 1 x 20-mmM61A1 (1,028) | 1 x 20-mmM61A1 (1,028) |
Payload | 5,443 kg | 6,350 kg | 6,350 kg |
Hardpoints | 5 | 5 | 5 |
AA Weapons | AIM-9 | AIM-9 | AIM-9 |
AS Weapons | LAU-3/18 M117 Mk 82/84 | AGM-12 LAU-3/18 M117 Mk 82/84 | AGM-45 AGM-78 |
Production | |||
Built | 75 | 610 | (54) |
Total | 833 |