Last site update: 03-10-2008

 

         

 

  

 

Rockwell B-1B Lancer

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Rockwell B-1B Lancer

After years of discussions, the Rockwell B-1B Lancer 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 Km/h.

 

Developing Nation: United States.
First Flight(s): December 23, 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:

87.091 kg.

Weight Max. Load: maximum take-off 216.367 kg.
Engines: four General Electric F101-GE-102.
Max. Speed: 1.328 km/h..
Max. Height: service ceiling 15.240 m.
Max. Range: 12.000 km.
Fuel and Load:

internal fuel 88.452 kg.

Maximum ordnance 34.020 kg internally.

And 26.762 kg externally.

Weapons:

AGM-69A SRAM-A (short-range attack missile).

AGM-86B ALCM   (air-launched cruise missile).

B61 or B83 nuclear bombs.

 

October 7, 2001 Afghanistan, Enduring Freedom.

 Air-to-ground strikes against Osama bin Laden's  Al-Quaida and the Taliban with cruise missiles.

 

The B-1B is only in use by the United States Air Force.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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