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Douglas
A-3 Skywarrior

General information
Type Strategic bomber
National origin United States
Manufacturer Douglas Aircraft Company
Status Retired
Primary user United States Navy
Number built 282
History
Manufactured 1956–1961
Introduction date 1956
First flight 28 October 1952
Retired 27 September 1991
Developed into Douglas B-66 Destroyer

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History
Douglas Aerospace Douglas A-3 Skywarrior
Manufactured 1956–1961 First flight 28 October 1952
  




The Douglas A-3 Skywarrior is a jet-powered strategic bomber that was developed and produced by the Douglas Aircraft Company. It was designed by Douglas on behalf of the United States Navy, which sought a carrier-capable strategic bomber. In July 1949, Douglas was awarded the contract to produce its design, having bested eight other aircraft companies' submissions. Unlike rival designs, which had aimed for a 100,000 lb (45,000 kg) maximum take-off weight, the Skywarrior was developed for a 68,000 lb (31,000 kg) take-off weight, facilitating its use from the navy's existing Midway-class aircraft carriers. Large portions of the aircraft were produced by the Westinghouse Electric Corporation, including its early Westinghouse J40 turbojet engines, which failed to meet promises and were replaced by the rival Pratt & Whitney J57 engine by mid-1953. On 28 October 1952, the prototype XA3D-1 performed the type's maiden flight.

Design

The Skywarrior had a 36° degree swept wing and two Pratt & Whitney J57 turbojet engines. Early prototypes had used the intended Westinghouse J40, a powerplant that proved to be disastrous and was subsequently canceled. The turbojets could be supplemented by a provision for twelve 4,500 lbf (20 kN) thrust JATO bottles. The aircraft had a largely conventional semi-monocoque fuselage, with the engines in underwing nacelles. Flight controls were hydraulic, and for storage below deck, the A-3's wings folded outboard of the engines, lying almost flat, and its vertical stabilizer was hinged to starboard. Capacious internal fuel tanks provided long range.

Camera arrangement of a camouflaged RA-3B of Heavy Photographic Squadron 61

Variants

EA-3B Skywarrior aboard museum ship USS Yorktown at Patriots Point Park in Charleston, South Carolina
  • XA3D-1: Two prototypes with Westinghouse J40 turbojets, no cannon in tail turret.
  • YA3D-1 (YA-3A): One pre-production prototype with Pratt & Whitney J57 engines. Later used for tests at the Pacific Missile Test Center.
  • A3D-1 (A-3A): 49 initial production versions, serving largely in developmental role in carrier service.
  • A3D-1P (RA-3A): One A3D-1 converted as a prototype for the A3D-2P with camera pack in the weapon bay.
  • A3D-1Q (EA-3A): Five A3D-1s converted for the electronic reconnaissance (ELINT) role, with ECM equipment and four operators in weapons bay.
  • A3D-2 (A-3B): Definitive production bomber version, with stronger airframe, more powerful engines, slightly larger wing area (812 ft2/75 m2 versus 779 ft2/72 m2), provision for in-flight refueling reel for tanker role. Final 21 built had new AN/ASB-7 bombing system, reshaped nose; deleted tail turret in favor of electronic warfare installation.

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Douglas Aircraft

Douglas Aerospace Douglas A-3 Skywarrior Manufactured 1956–1961
First flight 28 October 1952

1

General Info

      • Crew: 3
      • Length: 76 ft 4 in (23.27 m)
      • Wingspan: 72 ft 6 in (22.10 m)
      • Height: 22 ft 9.5 in (6.947 m)
      • Wing area: 812 sq ft (75.4 m2) with slats and CLE from A3D-2/A-3B
2

Powerplant

          • Empty weight:(17,876 kg)
          • Gross weight: (31,751 kg)
          • Max takeoff weight:(37,195 kg)
          • Powerplant: 2 × Pratt & Whitney J57-P-10 turbojet engines, 10,500 lbf (47 kN) thrust each dry
          12,400 lbf (55 kN) with water injection
plane
3

Performance

  • Maximum speed: 530 kn (610 mph, 980 km/h) at 10,000 ft (3,000 m)
  • Cruise speed: (600 mph, 960 km/h)
  • Range: 1,825 nmi (2,100 mi, 3,380 km)
  • Ferry range: 4,670 km
  • Service ceiling: 41,000 ft (12,000 m)
  • g limits: +3.4
4

Armament

    • Guns: 2 × 20 mm M3L cannon in the tail turret
    • Bombs: 12,800 pounds (5,800 kg) of free-fall bombs or mines,[including any combination of[
      • 12 × 500 pounds (230 kg) Mark 82 bombs or
      • 6 × 1,000 pounds (450 kg) Mark 83 bombs or
      • 8 × 1,600 pounds (730 kg) armor-piercing bombs or
      • 4 × 2,000 pounds (910 kg) bombs
Special Links McDonnell Douglas

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When ordering the XA3D-1 the Navy had specified that the aircraft should be powered by Westinghouse J40s. Accordingly, Douglas fitted two 7,000 lb. (3,175 kg) thrust XJ40-WE-3 engines to the XA3D-1 and proposed using 7,500 lb. (3,402 kg) J40-WE-12s on the production A3D-1 Skywarriors.

Douglas
A-6 Skywarrior

Ed Heinemann, always weight conscious, strove even harder to keep the aircraft weight well below the 100,000 lb. limit.

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In 1937, the United States Army Air Corps wanted to acquire increased firepower, both in terms of ground bombing and support

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