A2D Skyshark

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A2D Skyshark
Type Attack aircraft
Manufacturer Douglas Aircraft Company
Designed by Ben Collins
Maiden flight 1950
Status Cancelled
Primary user United States Navy
Number built 12 (4 never flew)
Developed from A-1 Skyraider

The Douglas A2D Skyshark was a turboprop-powered attack aircraft built by the Douglas Aircraft Company for the United States Navy.

Contents

[edit] Development

In 1947 the Navy issued a letter of intent to Douglas Aircraft for a turboprop to be carrier-based. The need to operate from Casablanca class escort carriers dictated the use of a turboprop instead of jet power.[1] The advantages of turboprop engines over piston was in power to weight ratio and the maximum power that could be practically generated. The advantage over jets was that a turboprop ran at near full RPM all the time, and thrust could be quickly generated by simply changing the propeller pitch. While resembling the AD Skyraider, the A2D was an entirely different airplane. Engine development problems delayed the first flight until May 1950. Allison failed to deliver a "production" engine until 1953, and while testing an XA2D with that engine, test pilot C. G. "Doc" Livingston pulled out of a dive and was surprised by a loud noise and pitch up. His windscreen was covered with oil and the chase pilot told Livingston that the propellers were gone. The gearbox had failed. Livingston successfully landed the airplane. By the summer of 1954, the A4D was ready to fly. The escort carriers were being mothballed, and time had run out for the troubled A2D program.[2] Due largely to the failure of the Allison T40 program to produce a reliable engine, the Skyshark never entered operational service.

Twelve Skysharks were built. Most were scrapped or destroyed in accidents, and only one is believed to have survived. One was sighted at the airport at Idaho Falls, Idaho, in September 2006,[citation needed] and appeared to be in airworthy condition.

[edit] Specifications (XA2D-1)

Data from Encyclopedia of American Aircraft[3]

General characteristics

  • Crew: 1
  • Length: 41 ft 3 in (12.58 m)
  • Wingspan: 50 ft 0 in (15.24 m)
  • Height: 17 ft 1 in (3.68 m)
  • Wing area: 400 ft² (37 m²)
  • Empty weight: 12,900 lb (5,864 kg)
  • Loaded weight: 18,700 lb (8,500 kg)
  • Max takeoff weight: 22,960 lb (10,436 kg)
  • Powerplant:Allison XT-40-A-2 turboprop, 5,100 shp (3,800 kW)

Performance

Armament

  • Guns:20 mm (0.787 in) T31 cannon
  • Other: up to 5,500 lb (2,500 kg) on 3 external hardpoints

[edit] References

[edit] Notes

  1. ^ Heinemann and Rausa 1980, p. 177.
  2. ^ Heinemann and Rausa 1980, p. 183.
  3. ^ Baugher, Joe (2001-10-24). Douglas XA2D-1 Skyshark. Encyclopedia of American Aircraft.

[edit] Bibliography

  • Heinemann, Edward, H. and Rausa, Rosario. Combat Aircraft Designer. London: Jane's Publishing Co., 1980. ISBN 0-7106-0040-2.
  • Markgraf, Gerry. Douglas Skyshark, A2D Turbo-Prop Attack (Naval Fighters Number Forty-Three). Simi Valley, CA: Ginter Books, 1997. ISBN 0-942612-43-4.

[edit] See also

Related development

Comparable aircraft

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