F4D Skyray

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F4D (F-6) Skyray
F4D-1 Skyray
Type Fighter aircraft
Manufacturer Douglas Aircraft Company
Maiden flight 23 January 1951
Introduced 1956
Retired 1964
Primary users United States Navy
United States Marine Corp
Number built 422
Variants F5D Skylancer

The American Douglas F4D Skyray (later redesignated F-6 Skyray) was a carrier-based fighter built by the Douglas Aircraft Company. Although it was in service for a very short time and never entered combat, it was notable for being the first carrier-launched plane to hold the world's absolute speed record and was the first Navy fighter capable of exceeding Mach 1 in level flight.

Contents

The F4D Skyray was a wide delta wing design with long, sharply swept, rounded wings. The thick wing roots contained the air intakes feeding a single turbojet. Fuel was contained both in the wings and the deep fuselage. Leading-edge slats were fitted for increased lift during takeoff and landing, while the trailing edges were mostly elevon control surfaces. Additional pitch trimmers were fitted inboard near the jet exhaust, and were locked upward on takeoff and landing.

F4D-1 of VF-74 on the USS Franklin D. Roosevelt
F4D-1 of VF-74 on the USS Franklin D. Roosevelt

The Westinghouse J40 turbojet was the intended power plant, but Douglas fortunately took a conservative view and gave options for other powerplants. The J40 proved troublesome and was eventually cancelled, and the Skyray was fitted instead with the Pratt & Whitney J57, a more powerful but larger engine.

Production aircraft were not delivered until early 1956, while the U.S. Marine Corps received their first in 1957. In total, 419 F4D-1 (later designated F-6 in the unified designation system) aircraft were produced.

Its unique and notable looks also played a part in making the Skyray one of the best-remembered early jet fighters. Affectionately known as the "Ford" (after the "Four" and "D" of its designation), this aircraft had a spectacular rate and angle of climb and set a new time to altitude record. It saw the Skyray fly from a complete stop to 50,000 feet/15,000 meters in 2 minutes and 36.05 seconds, all while flying at a 70 degree pitch angle.

In April 1956 VC-3 was the first squadron operational with the F4D-1. It was later redesignated VFAW-3 and assigned to NORAD, as the only US Navy-squadron. VFAW-3 was permanently based at NAS North Island, San Diego. The following Navy-squadrons flew the F4D-1: VFAW-3, VF-13, VF-23, VF-51, VF-74, VF-101, VF-102, VF-141, VF-162, VF-213, VF-881 and VF-882. The US Marine Corps also flew the Skyray, squadrons VMF-113, VMF-114, VMF-115, VMF-215, VMF-314, VMF-513, VMF-513 and VMF(AW)-542. When the Skyray was redesignated F-6A in September 1962, only VFAW-3, VMF-114, VMF-513 and VMF(AW)-542 flew the type together with the reserve squadrons VMF-215, VF-881 and VF-882. The last operational squadron was VMF(AW)-542 which used the Skyray until February 1964.

APQ-50A radar of a F4D-1
APQ-50A radar of a F4D-1

The Skyray was designed exclusively for the high-altitude interception role and was unsuited to the multi-mission capabilities soon in demand, so it had a short life in Navy and Marine Corps service, the last aircraft being withdrawn from service in 1964. A single aircraft was used by NACA (soon to be NASA) until 1969.

A derived successor, the F5D Skylancer, was designed and prototypes were built, but it was cancelled as too similar in mission parameters to the Vought F8U Crusader and also to reduce dependence upon Douglas Aircraft, which was also producing several other aircraft for the US Navy.[citation needed]

XF4D-1
Prototypes, redesignated YF-6A in 1962, two built
F4D-1
Single-seat fighter aircraft, production model redesignated F-6A in 1962, 420 built.
F4D-2
Re-engined F4D-1 with the J57-F-14, 100 on order cancelled.
F4D-2N
F4D-2 version with extended nose housing twin radar scanners, project only evolved into the F5D Skylancer.
YF-6A
XF4D-1 prototypes redesignated in 1962.
F-6A
F4D-1 redesignated in 1962.

With the new joint services designations the Navy/Marine designations were replaced (which included a manufacture letter code), the F4D was redesignated the F-6A. The lower numbers were due to the fighter series being reset back to F-1 (after having gone up to F-111) under the 1962 United States Tri-Service aircraft designation system.

Possible confusion: The F4D (old designation) should not be confused with the F-4D (new designation) - the latter being the "D" variant of the McDonnell F-4 Phantom II.

Flag of the United States United States

General characteristics

  • Crew: 1
  • Length: 33 ft 6 in (10.21 m)
  • Wingspan: 45 ft 3 in (13.8 m)
  • Height: 13 ft 0 in (3.96 m)
  • Wing area: 557 ft² (52 m²)
  • Empty weight: 16,024 lb (7,268 kg)
  • Loaded weight: 22,648 lb (10,273 kg)
  • Max takeoff weight: 27,116 lb (12,300 kg)
  • Powerplant:Pratt & Whitney J57-P-8, -8A or -8B turbojet
    • Dry thrust: 10,200 lbf (45 kN)
    • Thrust with afterburner: 16,000 lbf (71 kN)

Performance

Armament

  • Guns: 4× 20 mm (0.787 in) Mk 12-0 cannons in wing roots, 65 rounds/gun
  • Rockets:
    • 6 pods of 7× 2.75 in (70 mm) unguided rockets or
    • 4 pods of 19× 2.75 (70 mm) unguided rockets
  • Missiles:AIM-9 Sidewinder air-to-air missiles
  • Bombs: 2× 2,000 lb (910 kg) bombs

Avionics

Notes
  1. ^ http://www.naa.aero/ National Aeronautics Association, keeper of the Collier Trophy]
Bibliography
  • Green, William and Pollinger, Gerald. The Aircraft of the World. London: Macdonald, 1955.
  • Winchester, Jim. Fighter - The World's Finest Combat Aircraft - 1913 to the Present Day. New York: Barnes & Noble Publishing, Inc. and Parragon Publishing, 2006. ISBN 0-7607-7957-0.

Related development

Comparable aircraft

Designation sequence

Related lists

See also

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