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Republic F-105 Thunderchief Fighter Bomber |
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DESCRIPTION:
The F-105 was a rugged fighter bomber that saw a great deal of action in the Vietnam War. The design was notable in many respects, including its large bomb-bay, unique forward-swept engine inlets at the wing root, and the fact that it remains the largest single-seat combat aircraft ever built. Also called the 'Ultra Hog,' 'Lead Sled,' and 'Thud,' by its pilots, the Thundechief was originally intended to be a long-range tactical nuclear bomber operating at high speed and altitude. During the Vietnam War, however, the F-105 was used extensively as a conventional attack aircraft striking deep within enemy territory. Later F-105G models were also modified as the first dedicated defense-suppression 'Wild-Weasel' aircraft. The F-105 began entering service in 1958 and was not withdrawn from front-line service until 1982. The final operational flight occurred in 1984.
Data below for F-105F/G |
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| HISTORY: | |
| First Flight |
(YF-105A) 22 October 1955 (F-105B) 26 May 1956 (F-105F) 11 June 1963 |
| Service Entry | August 1958 |
| Retirement |
25 February 1984
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CREW:
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(B,D) 1 pilot, (F,G) one pilot and one systems officer
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ESTIMATED COST:
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(F-105D) $2.2 million
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| AIRFOIL SECTIONS: | |
| Wing Root | NACA 65A005.5 |
| Wing Tip |
NACA 65A003.7
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| DIMENSIONS: | |
| Length | 69.63 ft (21.21 m) |
| Wingspan | 34.94 ft (10.65 m) |
| Height | 20.17 ft (6.15 m) |
| Wing Area | 384.3 ft2 (35.77 m2) |
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Canard Area
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not applicable
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| WEIGHTS: | |
| Empty | 28,393 lb (12,879 kg) |
| Normal Takeoff | unknown |
| Max Takeoff | 54,000 lb (24,495 kg) |
| Fuel Capacity |
internal: unknown external: unknown |
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Max Payload
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14,000 lb (6,350 kg)
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| PROPULSION: | |
| Powerplant | one Pratt & Whitney J75-19W afterburning turbojet |
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Thrust
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24,500 lb (109.0 kN)
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| PERFORMANCE: | |
| Max Level Speed |
at altitude: 1,390 mph (2,235 km/h) at 36,000 ft (10,975 m), Mach 2.1 at sea level: unknown |
| Initial Climb Rate | 32,000 ft (9,750 m) / min |
| Service Ceiling | 52,000 ft (15,850 m) |
| Range |
typical: 400 nm (740 km) ferry: 2,080 nm (3,850 km) |
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g-Limits
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unknown
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| ARMAMENT: | |
| Gun | one 20-mm M-61A1 cannon (1,029 rds) |
| Stations | one internal weapons bay and five external hardpoints |
| Air-to-Air Missile | up to four AIM-9 Sidewinder |
| Air-to-Surface Missile | AGM-12 Bullpup, AGM-45 Shrike (G only) |
| Bomb | various nuclear bombs, up to two 3,000-lb bombs, up to five 1,000-lb bombs, up to 16 750-lb bombs, Mk 77 Napalm |
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Other
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ECM pods, 2.75-in rocket pods
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| KNOWN VARIANTS: | |
| YF-105A | Original prototype, never went into production |
| YF-105B | Improved prototype with upgraded engine and a new fuselage shape dictated by the "area-rule" |
| F-105B | First production one-seat fighter bomber; 71 built |
| RF-105B | Proposed reconnaissance model, not built |
| JF-105B | Test aircraft re-built from RF-105B airframes; 3 converted |
| F-105C | Proposed two-seat trainer, not built |
| F-105D | One-seat all-weather fighter bomber with a new radar and navigation equipment, improved engine, and better avionics; 600 built |
| RF-105D | Proposed reconnaissance model, not built |
| F-105E | Proposed two-seat trainer based on the F-105D model, not built |
| F-105F | Two-seat combat-capable trainer; 143 built |
| EF-105F | Re-built F-105F models equipped with radar homing and jamming equipment; 86 converted |
| F-105G |
Two-seat defense suppression model with electronic countermeasures, radar homing, and jamming equipment; 60
EF-105F models rebuilt as F-105G variant
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| KNOWN COMBAT RECORD: |
Vietnam War (USAF, 1965-1972)
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| KNOWN OPERATORS: |
United States (US Air Force) United States (US Air Force Reserves) United States (US Air National Guard) |
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3-VIEW SCHEMATIC:
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SOURCES:
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