Vought F-8 Crusader
The Vought F-8 Crusader (or F8U) was an American single-engine, supersonic jet aircraft built by Vought and used by the US Navy and Marines.
Vought F-8 Crusader - WW2 American Aircraft & Warplanes, Info

Time Period: Post-WW2
Country of Origin: United States
Type: Fighter Aircraft
Manufacturer: Vought

Vought F-8 Crusader Aircraft Overview

The Vought F-8 Crusader is a supersonic carrier-based fighter aircraft that was used by the United States Navy and the United States Marine Corps from the late 1950s through the 1970s. It was designed as a single-seat, all-weather aircraft that could operate from aircraft carriers and perform a variety of missions, including air superiority, ground attack, and reconnaissance.

The F-8 Crusader was developed by Vought Aircraft Industries in the late 1950s to replace the F-7 Cutlass. It featured a distinctive variable-incidence wing that could be adjusted in flight to provide increased lift and reduced drag. The aircraft was powered by a single Pratt & Whitney J57 turbojet engine, which gave it a top speed of Mach 1.8 and a range of over 1,000 miles.

The F-8 Crusader was armed with four 20mm Colt Mk 12 cannons and could carry a variety of missiles and bombs, including the AIM-9 Sidewinder air-to-air missile and the Zuni air-to-ground rocket. It was also equipped with a reconnaissance camera, which allowed it to perform photo-reconnaissance missions.

The F-8 Crusader saw extensive service during the Vietnam War, where it was used for air superiority missions and ground attack missions. It was known for its speed, maneuverability, and reliability, and it was credited with shooting down several enemy aircraft. The aircraft was eventually replaced by the F-14 Tomcat in the late 1970s, but it remains a popular aircraft among aviation enthusiasts and is remembered as an important part of the history of military aviation.

Vought F-8E Specifications

  • Crew: 1
  • Length: 55 ft 11.6 in (17.059 m) 
  • Wingspan: 35 ft 8 in (10.87 m)
  • Height: 15 ft 9.1 in (4.803 m) 
  • Wing area: 375 sq ft (34.8 m2)
  • Aspect ratio: 3.4
  • Airfoil: root: NACA 65A006 mod; tip: NACA 65A005 mod
  • Zero-lift drag coefficient: CD0.0133
  • Drag area: 5.0 sq ft (0.46 m2)
  • Empty weight: 18,800 lb (8,528 kg) 
  • Gross weight: 29,000 lb (13,154 kg)
  • Max takeoff weight: 34,000 lb (15,422 kg)
  • Fuel capacity: 1,348 US gal (1,122.4 imp gal; 5,102.7 L)
  • Powerplant: 1 × Pratt & Whitney J57-P-20A afterburning turbojet engine, 11,400 lbf (51 kN) thrust dry, 18,000 lbf (80 kN) with afterburner

Vought F-8E Performance

  • Maximum speed: 1,066 kn (1,227 mph, 1,974 km/h) at 36,000 ft (10,973 m)
  • Maximum speed: Mach 1.8
  • Cruise speed: 268 kn (308 mph, 496 km/h) 
  • Stall speed: 135 kn (155 mph, 250 km/h) 
  • Never exceed speed: 775 kn (892 mph, 1,435 km/h) 
  • Combat range: 394 nmi (453 mi, 730 km)
  • Ferry range: 1,507 nmi (1,734 mi, 2,791 km) with external fuel
  • Service ceiling: 58,000 ft (18,000 m)
  • Lift-to-drag: 12.8
  • Wing loading: 77.3 lb/sq ft (377 kg/m2)
  • Thrust/weight: 0.62

Vought F-8E Armament

  • Guns: 4× 20 mm (0.79 in) Colt Mk 12 cannons in lower fuselage, 125 rpg
  • Hardpoints: 2× side fuselage-mounted Y-pylons (for mounting AIM-9 Sidewinders and Zuni rockets) and 2× underwing pylon stations with a capacity of 4,000 lb (2,000 kg), with provisions to carry combinations of:
    • Rockets: 2× LAU-10 rocket pods (each with 4× 5 inch (127mm) Zuni rockets)
    • Missiles:
      • 4× AIM-9 Sidewinder or Matra Magic (French Navy only) air-to-air missiles
      • 2× AGM-12 Bullpup air-to-surface missiles
    • Bombs:
      • 8× 250 lb (113 kg) Mark 81 bombs or
      • 8× 500 lb (227 kg) Mark 82 bombs or
      • 2× 1,000 lb (454 kg) Mark 83 bombs or
      • 2× 2,000 lb (907 kg) Mark 84 bombs

Vought F-8 Crusader Image Gallery

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