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| Huff-Daland XB-1
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| Description
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| Role | Heavy bomber
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| Crew | 5
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| First Flight |
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| Entered Service | n/a
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| Manufacturer | Huff-Daland (later Keystone)
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| Number built | 1 XB-1 (later cv. to XB-1B)
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| Dimensions
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| Length | 61 ft 6 in | 18.7 m
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| Wingspan | 85 ft | 25.9 m
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| Height | 19 ft 3 in | 5.9 m
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| Wing area | ft² | m²
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| Weights
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| Empty | lb | kg
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| Loaded | lb | kg
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| Maximum takeoff | lb | kg
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| Capacity |
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| Powerplant
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| Engines | Packard 2A-1530 (2)
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| Curtiss V-1570-5 (2)
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| Power | 510 hp | 380 kW
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| Performance
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| Maximum speed | 100 mph | 161 km/h
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| Cruising speed | mph | km/h
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| Combat range | 700 miles | 1,126.3 km
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| Ferry range | miles | km
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| Service ceiling | 15,000 ft | 4,572 m
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| Rate of climb | ft/min | m/min
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| Wing loading | lb/ft² | kg/m²
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| Armament
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| Guns | .30-calibre (7.62 mm) machine guns
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| Bombs | 2,500lb (1,134 kg) 4,000 lb (1,814 kg) on short runs
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The Huff-Daland XB-1 was a prototype bomber aircraft built for the United States Army.
The first aircraft named using just a B- designation. Prior to 1926, the U.S. Army used LB- and HB- prefixes, signifying 'Light Bomber' and 'Heavy Bomber'. The first XB-1, called the Super-Cyclops by Huff-Daland, was an extension of the earlier Huff-Daland XHB-1 'Cyclops'. It was essentially the same in size, but sported a twin tail and twin engines.
The original Packard engines did not provide enough power for the plane. Consequently, Huff-Daland (now renamed Keystone) made a new version of the plane, dubbed the XB-1B, which utilised more powerful Curtiss Aircraft 'Conqueror' engines. The sole XB-1 was converted to an XB-1B
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