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  • Vought F-8 Crusader Carrier-Borne Naval Fighter Aicraft

    The storied Vought F-8 Crusader carrier-based fighter served in an operational role for over 40 years with the United States, the Philippines, and France.

     Updated: 4/21/2017; Authored By Staff Writer; Content ¬©www.MilitaryFactory.com

    The Vought F-8 "Crusader" was a direct response to a United States Navy requirement for a modern supersonic, carrier-based fighter. Utilizing nearly the identical powerplant of the North American F-100 "Super Sabre", the F-8 Crusader became the world's first carrier-based aircraft to break the speed of sound. The single-seat Crusader featured a long fuselage with a swept-back high-wing assembly and single-engine installation. A single vertical tail fin was fitted over the rear of the fuselage. The engine, exhausting through a large jet pipe at rear, generated upwards of 18,000lb thrust with an afterburn capability. As a naval carrier-based fighter, the aircraft was fitted primarily with 4 x 20mm internal cannons for close-in work and supported early forms of American air-to-surface missiles (no ground attack capability was added) including the AIM-9 Sidewinder short-range missile. Crusaders were eventually pressed into service over the skies of Vietnam with the growing American commitment in Southeast Asia. There it served with both the United States Marine Corps (USMC) and the United States Navy (USN).

    As a predominantly cannon-armed fighter, the F-8 has been seen by many as the end of the line for all-cannon-armed fighter jets - making the F-8 the last of the classic "gunfighters".

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    Vought F-8 Crusader Technical Specifications

    Service Year: 1957
    Type: Carrier-Borne Naval Fighter Aicraft
    National Origin: United States
    Manufacturer(s): Vought - USA
    Production Total: 1,219

    Structural (Crew Space, Dimensions and Weights)

    Operating Crew: 1
    Length: 54.49 feet (16.61 meters)
    Width: 35.17 feet (10.72 meters)
    Height: 15.75 feet (4.80 meters)

    Weight (Empty): 19,925 lb (9,038 kg)
    Weight (MTOW): 34,000 lb (15,422 kg)

    Installed Power and Standard Day Performance

    Engine(s): 1 x Pratt & Whitney J57-P-20A turbojet engine with afterburning developing 18,000 lb of thrust.

    Maximum Speed: 1,118 mph (1,800 kph; 972 knots)
    Maximum Range: 600 miles (966 km)
    Service Ceiling: 58,704 feet (17,893 meters; 11.12 miles)
    Rate-of-Climb: 19,000 feet-per-minute (5,791 m/min)

    Armament / Mission Payload

    4 x 20mm internal cannons

    Mission-specific armament included:
    2 OR 4 x AIM-9 Sidewinder air-to-air missiles
    2 x AGM12 Bullpup air-to-surface missiles

    French Naval Variant:
    4 x 20mm cannons
    2 x Matra R.530 air-to-air missiles
    4 x Matra Magic R.550 air-to-air missiles

    Global Operators / Customers

    France; Philippines; United States

    Model Variants (Including Prototypes)

    F8U-1 - Initial Production Model

    F8U-1P - Reconnaissance Variant

    F8U-1E - Limited All-Weather Model with improved radar system.

    F8U-2 - Improved radar system; Improved fire control system; Uprated J57-P-16 powerplant generating 16,900lbs of thrust with afterburn.

    F8U-2N - Updated avionics systems; Uprated J57-P-20 powerplant increasing thrust to 18,000lbs.

    F8U-2NE - Improved all-weather model with updated radar and fire control systems.

    F-8A - F8U-1 Model Redesignated

    F-8B - F8U-1E Model Redesignated

    F-8C - F8U-2 Model Redesignated

    F-8D - F8U-2N Model Redesignated

    F-8E - F8U-2NE Model Redesignated

    RF-8A - F8U-1P Model Redesignated

    F-8E(FN) - French Naval Export Version; blown flaps for reduced landing speeds and provision for French-based Matra air-to-air missile systems to replace AIM-9 Sidewinders.

    F-8P - Refurbished F-8H models exported to the Philippine Air Force.