Fighter Jets
Republic F-84 Thunderjet
ICAO: F84
Overview
Republic F-84F Thunderstreak — swept-wing fighter-bomberThe F-84F first flew in 1950 and entered service in 1954. Unlike the straight-wing Thunderjet, it adopted a swept-wing configuration for higher speeds. Structural refinements improved stability and handling.Powered by a Wright turbojet producing approximately 7,200 pounds of thrust (32 kN), the Thunderstreak exceeded 600 knots (1,111 km/h). Maximum takeoff weight surpassed 28,000 pounds (12,701 kg).The aircraft served extensively in Europe during the Cold War. It fulfilled tactical strike roles until replaced by more advanced supersonic fighters. The F-84F marked a transition toward swept-wing jet designs.
Live Fleet Activity (F84F)
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Specifications
Units
- Engine
- 1 × Wright J65-W-3
- Engine type
- Jet
- Thrust
- 7,220 lbf · 32 kN
- Avionics
- A-1CM or A-4 gunsight with APG-30 or MK-18 ranging radar
- Wing tips
- No winglets
- Seats
- 1
- Crew
- —
- Cabin width
- —
- Cabin height
- —
- Cabin length
- —
- Exterior length
- 43 ft 5 in · 13.23 m
- Tail height
- 14 ft 5 in · 4.40 m
- Fuselage diameter
- 4 ft 3 in · 1.30 m
- Wing span
- 33 ft 8 in · 10.25 m
- Baggage volume
- —
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 28,000 lb · 12,700 kg
- Max landing weight
- —
- Max payload
- 6,600 lb · 3,000 kg
- Fuel capacity
- 850 gal · 3,200 L · 2,600 kg (Jet A)
- Max cruise speed
- 604 kt · 695 mph · 1,119 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- 137 kt · 158 mph · 254 km/h
- Range
- 704 nm · 810 mi · 1,300 km
- Fuel burn
- —
- Ceiling
- 46,000 ft · 14,000 m
- Rate of climb
- 8,200 ft/min · 42 m/s
- Takeoff distance
- —
- Landing distance
- —
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Operational Context
Development of the F-84F began in 1948 when the manufacturing company Republic Aviation designed a swept-wing variant of the F-84 intended to compete with the performance of the F-86 Sabre. The aircraft prototype was given the designation XF-96A and took to the air for the first time on June 3, 1950, piloted by Otto P. Haas. In July 1950, the aircraft was designated as F-84F Thunderstreak and was ordered into production.
The F-84F is a single-crew fighter with an external length of 13.23 meters, an external height of 3 meters, and a fuselage diameter of 1.3 meters. It has a tail height of 4.4 meters and a wheelbase of 5.8 meters. The swept wing has a wingspan of 10.25 meters and a wing area of 30 square meters. It has an empty weight of 5,200 kg, a maximum takeoff weight of 12,701 kg, a maximum payload of 3,000 kg, and a fuel tank capacity of 847 US gallon.
The aircraft is powered by a single Wright J65-W-3 engine. It is an axial-flow turbojet with a thirteen-stage axial compressor, annular combustors, and a two-stage axial turbine. It produces a maximum takeoff thrust of 7,220 lbf. The F-84F has a maximum speed of 604 knots at sea level and a combat range of 704 nautical miles with two drop tanks. It can fly up to 46,000 feet and can climb at a rate of 8,200 feet per minute.
The Thunderstreak could be armed with six 12.7 mm Browning M3 machine guns; four mounted in the nose over intake and two mounted in the wing roots, with 1,800 rounds in total. It is also armed with up to 2,727 kg of rockets and bombs including one Mark 7 nuclear bomb. The aircraft was fitted with A-1CM or A-4 gunsight with APG-30 or MK-18 ranging radar and includes several communications equipment such as AN/ARC-33 or 34 command set radio and AN/APX-6 or 6A instrument friend or foe set.
Sources and references used for research and fact-checking.