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A-7 Corsair II - From The Vought F-8 Crusader To The LTV A-7 | Aviation History
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The LTV A-7 Corsair II (Ling-Temco-Vought), a United States Attack Aircraft, and its evolution from Vought F-8 Crusader.
The evolution from the Vought F-8 Crusader to the LTV A-7 Corsair II marked a significant transition in the realm of carrier-based naval aviation, reflecting the changing requirements and technological advancements of the mid-20th century.
The Vought F-8 Crusader, first introduced in the late 1950s, was a supersonic, single-seat fighter aircraft designed for the United States Navy. Renowned for its exceptional speed and climb rate, the F-8 earned the nickname "The Last of the Gunfighters" due to its combination of advanced radar and cannon armament. The F-8 was a crucial component of naval air power during its time, serving as both an interceptor and a reconnaissance platform. Its unique feature, the variable-incidence wing, allowed for exceptional high-speed performance and effective takeoffs and landings from aircraft carriers.
As the needs of naval aviation evolved, there arose a demand for a more versatile aircraft that could fulfill a variety of roles, including ground-attack missions. This led to the development of the LTV A-7 Corsair II, which was intended as a multi-role aircraft capable of delivering precision strikes against ground targets. The A-7 retained some design elements from its predecessor, such as the delta wing configuration, but incorporated several new features to enhance its ground-attack capabilities.
Introduced in the late 1960s, the A-7 Corsair II featured a robust airframe, modern avionics, and the capacity for carrying a significant payload of bombs and missiles. Its design prioritized ease of maintenance and operational flexibility, making it well-suited for the demands of carrier-based operations. The A-7's sophisticated avionics included a computerized navigation and weapons delivery system, which significantly improved accuracy in strike missions.
The evolution from the F-8 Crusader to the A-7 Corsair II showcased a shift in focus from air superiority to multi-role capabilities, reflecting the changing nature of military conflicts and the need for adaptable aircraft. The A-7 Corsair II became a workhorse for the U.S. Navy and Air Force, demonstrating its effectiveness in various conflicts, including the Vietnam War and the Gulf War. Its legacy endured for decades, highlighting the success of the evolutionary process that transformed naval aviation from a dedicated fighter platform to a versatile multi-role aircraft.
General characteristics (A-7)
Crew: 1
Length: 46 ft 2 in (14.06 m)
Wingspan: 38 ft 9 in (11.8 m)
Width: 23 ft 9 in (7.24 m) wings folded
Height: 16 ft 1 in (4.9 m)
Wing area: 374.9 sq ft (34.83 m2)
Airfoil: NACA 65A007 root and tip
Empty weight: 19,127 lb (8,676 kg)
Max takeoff weight: 41,998 lb (19,050 kg) overload condition.
Fuel capacity: 1,338 US gal (5,060 L; 1,114 imp gal) (10,200 lb (4,600 kg)) internal
Powerplant: 1 × Allison TF41-A-2 non-afterburning turbofan engine, 15,000 lbf (66.7 kN) thrust
Performance
Maximum speed: 600 kn (690 mph, 1,100 km/h) at sea level
562 kn (1,041 km/h; 647 mph) at 5,000 ft (1,500 m) with 12x Mk82 bombs
595 kn (1,102 km/h; 685 mph) at 5,000 ft (1,500 m) after dropping bombs
Range: 1,070 nmi (1,231 mi, 1,981 km) maximum internal fuel
Ferry range: 1,342 nmi (1,544 mi, 2,485 km) with maximum internal and external fuel
Service ceiling: 42,000 ft (13,000 m)
Rate of climb: 15,000 ft/min (76.2 m/s)
Wing loading: 77.4 lb/sq ft (378 kg/m2)
Thrust/weight: 0.50 (full internal fuel, no stores)
Sustained maneuvering performance: 5,300 ft (1,600 m) turning radius at 4.3g and 500 kn (930 km/h; 580 mph) at an All Up Weight (AUW) of 28,765 lb (13,048 kg)
Take-off run: 1,705 m (5,594 ft) at 42,000 lb (19,000 kg)
Armament
Guns: 1× M61A1 Vulcan 20 mm (0.79 in) rotary cannon with 1,030 rounds
Hardpoints: 6× under-wing and 2× fuselage pylon stations (for mounting AIM-9 Sidewinder AAMs only) with a capacity of 15,000 lb (6,800 kg) total capacity, with provisions to carry combinations of:
Rockets: 4× LAU-10 rocket pods (each with 4× 127 mm (5.00 in) Zuni rockets)
Missiles:
2× AIM-9 Sidewinder air-to-air missile
2× AGM-45 Shrike anti-radiation missile
2× AGM-62 Walleye TV-guided glide bomb
2× AGM-65 Maverick air-to-ground missile
2× AGM-88 HARM anti-radiation missile
2× GBU-8 HOBOS electro-optically guided glide bomb
#aircraft #A7Corsair #aviation
The evolution from the Vought F-8 Crusader to the LTV A-7 Corsair II marked a significant transition in the realm of carrier-based naval aviation, reflecting the changing requirements and technological advancements of the mid-20th century.
The Vought F-8 Crusader, first introduced in the late 1950s, was a supersonic, single-seat fighter aircraft designed for the United States Navy. Renowned for its exceptional speed and climb rate, the F-8 earned the nickname "The Last of the Gunfighters" due to its combination of advanced radar and cannon armament. The F-8 was a crucial component of naval air power during its time, serving as both an interceptor and a reconnaissance platform. Its unique feature, the variable-incidence wing, allowed for exceptional high-speed performance and effective takeoffs and landings from aircraft carriers.
As the needs of naval aviation evolved, there arose a demand for a more versatile aircraft that could fulfill a variety of roles, including ground-attack missions. This led to the development of the LTV A-7 Corsair II, which was intended as a multi-role aircraft capable of delivering precision strikes against ground targets. The A-7 retained some design elements from its predecessor, such as the delta wing configuration, but incorporated several new features to enhance its ground-attack capabilities.
Introduced in the late 1960s, the A-7 Corsair II featured a robust airframe, modern avionics, and the capacity for carrying a significant payload of bombs and missiles. Its design prioritized ease of maintenance and operational flexibility, making it well-suited for the demands of carrier-based operations. The A-7's sophisticated avionics included a computerized navigation and weapons delivery system, which significantly improved accuracy in strike missions.
The evolution from the F-8 Crusader to the A-7 Corsair II showcased a shift in focus from air superiority to multi-role capabilities, reflecting the changing nature of military conflicts and the need for adaptable aircraft. The A-7 Corsair II became a workhorse for the U.S. Navy and Air Force, demonstrating its effectiveness in various conflicts, including the Vietnam War and the Gulf War. Its legacy endured for decades, highlighting the success of the evolutionary process that transformed naval aviation from a dedicated fighter platform to a versatile multi-role aircraft.
General characteristics (A-7)
Crew: 1
Length: 46 ft 2 in (14.06 m)
Wingspan: 38 ft 9 in (11.8 m)
Width: 23 ft 9 in (7.24 m) wings folded
Height: 16 ft 1 in (4.9 m)
Wing area: 374.9 sq ft (34.83 m2)
Airfoil: NACA 65A007 root and tip
Empty weight: 19,127 lb (8,676 kg)
Max takeoff weight: 41,998 lb (19,050 kg) overload condition.
Fuel capacity: 1,338 US gal (5,060 L; 1,114 imp gal) (10,200 lb (4,600 kg)) internal
Powerplant: 1 × Allison TF41-A-2 non-afterburning turbofan engine, 15,000 lbf (66.7 kN) thrust
Performance
Maximum speed: 600 kn (690 mph, 1,100 km/h) at sea level
562 kn (1,041 km/h; 647 mph) at 5,000 ft (1,500 m) with 12x Mk82 bombs
595 kn (1,102 km/h; 685 mph) at 5,000 ft (1,500 m) after dropping bombs
Range: 1,070 nmi (1,231 mi, 1,981 km) maximum internal fuel
Ferry range: 1,342 nmi (1,544 mi, 2,485 km) with maximum internal and external fuel
Service ceiling: 42,000 ft (13,000 m)
Rate of climb: 15,000 ft/min (76.2 m/s)
Wing loading: 77.4 lb/sq ft (378 kg/m2)
Thrust/weight: 0.50 (full internal fuel, no stores)
Sustained maneuvering performance: 5,300 ft (1,600 m) turning radius at 4.3g and 500 kn (930 km/h; 580 mph) at an All Up Weight (AUW) of 28,765 lb (13,048 kg)
Take-off run: 1,705 m (5,594 ft) at 42,000 lb (19,000 kg)
Armament
Guns: 1× M61A1 Vulcan 20 mm (0.79 in) rotary cannon with 1,030 rounds
Hardpoints: 6× under-wing and 2× fuselage pylon stations (for mounting AIM-9 Sidewinder AAMs only) with a capacity of 15,000 lb (6,800 kg) total capacity, with provisions to carry combinations of:
Rockets: 4× LAU-10 rocket pods (each with 4× 127 mm (5.00 in) Zuni rockets)
Missiles:
2× AIM-9 Sidewinder air-to-air missile
2× AGM-45 Shrike anti-radiation missile
2× AGM-62 Walleye TV-guided glide bomb
2× AGM-65 Maverick air-to-ground missile
2× AGM-88 HARM anti-radiation missile
2× GBU-8 HOBOS electro-optically guided glide bomb
#aircraft #A7Corsair #aviation
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