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Start | Rockwell | B-1A Lancer


General information


ManufacturerRockwell
ModelB-1A Lancer
ModificationB-1A
CountryUSA
Years1974
TypeBomber
Main rotor diameter-
Tail rotor diameter-
Wingspan-
Length45.78 m
Height10.24 m
Wing area-
Zero fuel weight-
Empty weight-
Maximum takeoff weight179170 kg
Normal takeoff weight176810 kg
Flight duration-
Engine4 General Electric F-101-GE-100
Power-
Thrust4 x 13500 kN
Maximum speed-
Cruising speed900-1040 km/h
Rate of climb-
Practical range9820 km
Service ceiling18300 m
Hovering ceiling-
Crew4
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