![]() |
|
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 |
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.
Ceiling
Combat RANGE
Aircraft Speed
Max Crew
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.
Ed Heinemann, always weight conscious, strove even harder to keep the aircraft weight well below the 100,000 lb. limit.
In 1937, the United States Army Air Corps wanted to acquire increased firepower, both in terms of ground bombing and support