The Rockwell B-1 Lancer is a four-engine variable-sweep wing supersonic heavy strategic bomber with a maximum weapon-payload of 125,000 lbs (56.700 kg) produced by the US-American manufacturer Rockwell International in operation with the United States Air Force.
Crew 4
Propulsion 4 Turbofan Engines
Engine Model General Electric F104-GE-102
Engine Power (each)
dry/with Afterburner 64,9 / 139,8 kN 14590 / 31428 lbf
Speed 1450 km/h 783 kts
901 mph
Service Ceiling 18.288 m 60.000 ft
Range 11.997 km 6.478 NM
7.455 mi.
Empty Weight 87.090 kg 192.000 lbs
max. Takeoff Weight 216.364 kg 477.000 lbs
Wing Span 41,67 m 136,7 ft
Wing Area 181,2 m² 1950 ft²
Length 44,81 m 147,0 ft
Height 10,36 m 34,0 ft
First Flight 23.12.1974
Production Status out of production
