B-52 Stratofortress
Specifications | ||||
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Primary Function: | Heavy bomber | |||
Contractor: | Boeing Military Airplane Co. | |||
Power Plant: | Eight Pratt & Whitney engines TF33-P-3/103 turbofan | |||
Thrust: | Each engine up to 17,000 pounds (7,650 kilograms) | |||
Length: | 159 feet, 4 inches (48.5 meters) | |||
Height: | 40 feet, 8 inches (12.4 meters) | |||
Wingspan: | 185 feet (56.4 meters) | |||
Speed: | 650 miles per hour (Mach 0.86) | |||
Ceiling: | 50,000 feet (15,151.5 meters) | |||
Weight: | Approximately 185,000 pounds empty (83,250 kilograms) | |||
Maximum Takeoff Weight: | 488,000 pounds (219,600 kilograms) | |||
Range: | Unrefueled 8,800 miles (7,652 nautical miles) | |||
Armament:
NOTE: The B-52 can carry 27 internal weapons. Authoritative sources diverge as to maximum munition loads, with some suggesting as many as 51 smaller munitions and 30 larger munitions, while others suggest maximum loads of 45 and 24, respectively. |
Approximately 70,000 pounds (31,500 kilograms) mixed ordnance -- bombs, mines and missiles.
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Systems |
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Crew: | Five (aircraft commander, pilot, radar navigator, navigator and electronic warfare officer) | |||
Accommodations: | Six ejection seats | |||
Unit Cost: | $30 million | |||
Date Deployed: | February 1955 | |||
Inventory: |
44 combat-coded Active force, 85; ANG, 0; Reserve, 9 |
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