Rockwell (Boeing) B-1b Lancer
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After years of discussions, the B-1B was introduced in the USAF in 1988.
After the project was cancelled by President Carter in June 1977, the Reagan administration decided in October 1981 to build a fleet of 100 B1-B’s for 28 billion Dollar.
Fitted with a “swept-wing” construction the B-1B is capable to perform attacks at low altitudes with speeds up to 960 Kph.
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Developing Nation: |
United States |
First Flight(s): |
December 23rd 1974 |
First operational: |
March 1988 |
Crew: |
4 |
Wing Span: |
41,67m spread, and 23,84m swept. |
Height: |
10,62 m |
Length: |
44,81 m |
Weight empty: |
87091 kg          |
Weight Max. Load: |
maximum take-off 216367 kg |
Engines: |
four General Electric F101-GE-102 |
Max. Speed: |
1328 km/h |
Max. Height: |
service ceiling 15240 m |
Max. Range: |
12000 km |
Fuel and Load: |
internal fuel 88452 kg Maximum ordnance 34020 kg internally And 26762 kg externally |
Weapons: |
AGM-69A SRAM-A (short-range attack missile) AGM-86B ALCMÂ Â (air-launched cruise missile) B61 or B83 nuclear bombs |
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October 7, 2001 Afghanistan, Enduring Freedom.  Air-to-ground strikes against Osama bin Laden’s Al-Quaida and the Taliban with cruise missiles. |
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The B-1B is only in use by the United States Air Force. |
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Research: Rob Vogelaar
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