Boeing B-52 Stratofortress
Boeing B-52 Stratofortress
In August 2014, the B-52 Stratofortress celebrated 60 years in the air. The eight-engine, 390,000-pound (176,901-kilogram) jet was America’s first long-range, swept-wing heavy bomber. It began as an intercontinental, high-altitude nuclear bomber, and its operational capabilities were adapted to meet changing defense needs.
B-52s have been modified for low-level flight, conventional bombing, extended-range flights and transport of improved defensive and offensive equipment — including ballistic and cruise missiles that can be launched hundreds of miles from their targets.
It had a rocky beginning. The original XB-52 design, selected by the Army Air Forces in 1946, was for a straight-wing, six-engine, propeller-powered heavy bomber. On Oct. 21, 1948, Boeing Chief Engineer Ed Wells and his design team were in Dayton, Ohio, when the Air Force’s chief of bomber development told them to scrap the propellers and come up with an all-jet bomber. Over the following weekend, in a Dayton hotel room, the team designed a new eight-engine jet bomber, still called the B-52, made a scale model out of balsa wood and prepared a 33-page report.
This effort impressed the Air Force’s Air Materiel Command, and the design was approved. As the war worsened in Korea, the Air Force, in 1951, designated the B-52 the country’s next intercontinental bomber and approved an initial production order for 13 B-52s. The first B-52A flew Aug. 5, 1954.
After assembly of three B-52As, production converted to B-52Bs, with more weight and larger engines. Some had photoreconnaissance or electronic capsules in their bomb bays and were redesignated RB-52Bs. The turbofan powered B-52H, the final version of the B-52, made its first flight March 6, 1961, and is still in service.
With each variant, the B-52 increased in range, power and capability. In all, 744 B-52s were produced by Seattle, Wash., and Wichita, Kan., plants between 1952 and 1962.
Throughout the 1950s, the B-52 chalked up many distance and speed records. It cut the round-the-world speed record in half, and in January 1962, flew 12,500 miles (20,117 kilometers) nonstop from Japan to Spain without refueling. This flight alone broke 11 distance and speed records. The B-52 saw active duty in the Vietnam War and was used in the Persian Gulf War in 1991 and over Afghanistan in 2001.
On Oct. 26, 2012, Boeing marked 50 years since it had delivered its last B-52 Stratofortress to the U.S. Air Force. H-model bomber 61-040 had been assigned to Minot Air Force Base, N.D., where it remained in active service. Modern engineering analyses showed the B-52’s expected lifespan extending beyond 2040.
In May 2014, The Air Force introduced the first B-52 aircraft upgraded with an advanced communications system developed by Boeing into its fleet. The Combat Network Communications Technology (CONECT) modification added several communication data links, full-color LCD displays with real-time intelligence feeds overlaid on moving maps, a state-of-the-art computing network, and the ability to retarget a weapon, or mission parameters, in flight. At that time, the Air Force operated 76 B-52s primarily out of Barksdale Air Force Base, La.; Minot Air Force Base, N.D., and Andersen Air Force Base, Guam, and planned to upgrade all of them.
- Crew: 5 (pilot, copilot, weapon systems officer, navigator, electronic warfare officer, and tail gunner until the removal of the tail gun in 1991)
- Length: 159 ft 4 in (48.5 m)
- Wingspan: 185 ft 0 in (56.4 m)
- Height: 40 ft 8 in (12.4 m)
- Wing area: 4,000 sq ft (370 m²)
- Airfoil: NACA 63A219.3 mod root, NACA 65A209.5 tip
- Empty weight: 185,000 lb (83,250 kg)
- Loaded weight: 265,000 lb (120,000 kg)
- Max. takeoff weight: 488,000 lb (220,000 kg)
- Fuel capacity: 47,975 U.S. gal (39,948 imp gal; 181,610 L)
- Zero-lift drag coefficient: 0.0119 (estimated)
- Drag area: 47.60 sq ft (4.42 m²)
- Aspect ratio: 8.56
- Powerplant: 8 × Pratt & Whitney TF33-P-3/103 turbofans, 17,000 lbf (76 kN) each
- Maximum speed: 560 kn (650 mph, 1,047 km/h)
- Cruise speed: 442 kn (525 mph, 844 km/h)
- Combat radius: 4,480 mi (3,890 nmi, 7,210 km)
- Ferry range: 10,145 mi (8,764 nmi, 16,232 km)
- Service ceiling: 50,000 ft (15,000 m)
- Rate of climb: 6,270 ft/min (31.85 m/s)
- Wing loading: 120 lb/ft² (586 kg/m²)
- Thrust/weight: 0.31
- Lift-to-drag ratio: 21.5 (estimated)
- Guns: 1× 20 mm (0.787 in) M61 Vulcan cannon originally mounted in a remote controlled tail turret on the H-model, removed from all current operational aircraft in 1991
- Bombs: Approximately 70,000 lb (31,500 kg) mixed ordnance; bombs, mines, missiles, in various configurations.
- Electro-optical viewing system that uses platinum silicide forward looking infrared and high resolution low-light-level television sensors
- ADR-8 chaff rocket (1965–1970)
- LITENING Advanced Targeting System
- Sniper Advanced Targeting Pod
- IBM AP-101 computer