B-23 Dragon
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| B-23 Dragon | |
|---|---|
 A B-23 Dragon on the airfield. |
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| Type | Medium bomber (in design) Multipurpose aircraft (in practice) |
| Manufacturer | Douglas Aircraft Company |
| Maiden flight | 27 July 1939 |
| Primary user | United States Army Air Force |
| Number built | 38 |
The Douglas B-23 Dragon was a twin-engined bomber developed by Douglas Aircraft Company as a successor to (and a refinement of) the B-18 Bolo.
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[edit] Design and development
The design of the B-23 was very similar to that of the Douglas DC-3. It was the first operational US bomber equipped with a glazed tail gun position. It first flew on July 27, 1939.
[edit] Operational history
While significantly faster and better armed than the B-18, the B-23 found itself inferior to newer bombers like the B-25 Mitchell and B-26 Marauder. For this reason, the 38 B-23s built were never used in combat. They worked in training, reconnaissance, transport (as the UC-67), and test-bed roles. One of the UC-67s is being restored to B-23 configuration by the National Museum of the United States Air Force.
The B-23's tall vertical tail was adapted by Ford for use on the B-24 Liberator and resulted in increased performance, but it was never adopted for production. The modification later became standard on the Navy's PB4Y Privateer, which was heavily derived from the Liberator.
After World War II, eccentric billionaire Howard Hughes converted a B-23 for use as his own personal transportation.
[edit] Operators
[edit] Specifications (B-23 Dragon)
Data from Joe Baugher's Encyclopedia of American aircraft[1]
General characteristics
- Crew: 6
- Length: 58 ft 6 in (17.8 m)
- Wingspan: 92 ft (28 m)
- Height: 18 ft 6 in (5.6 m)
- Wing area: 993 ft² (92.3 m²)
- Empty weight: 19,089 lb (8,677 kg)
- Loaded weight: 26,500 lb (12,000 kg)
- Max takeoff weight: 32,400 lb (14,700 kg)
- Powerplant: 2× Wright R-2600-3 radial engines, 1,600 hp (1,194 kW) each
Performance
- Maximum speed: 282 mph (245 knots, 454 km/h)
- Range: 1,400 mi (1,200 nm, 2,300 km) with 4,000 lb (1,800 kg) of bombs
- Service ceiling 31,600 ft (9,630 m)
- Rate of climb: 1,493 ft/min (7.6 m/s)
- Wing loading: 26.7 lb/ft² (130 kg/m²)
- Power/mass: 0.17 hp/lb (200 kW/kg)
Armament
- Guns:
- 3× 0.30 in (7.62 mm) machine guns
- 1× 0.50 in (12.7 mm) machine gun in tail turret
- Bombs: 4,000 lb (1,800 kg)
[edit] References
- ^ Baugher, Joe. B-23 "Dragon". 2000. Retrieved on 2005-01-03.
[edit] External links
[edit] See also
Related development
Comparable aircraft
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