B-1B `Lancer'
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General Specifications
Contractor : Rockwell International
Nation of origin : USA
Function : Low-Level bomber
Crew : 4
Date of introduction : 1974
In-service year : 1985
Dimensions
Wing span :
@ 15 degrees : 41.67m / 136
ft 9 in
@ 67.5 degrees : 23.84m / 78
ft 3 in
Length : 44.81m / 147 ft
Height : 10.36m / 34 ft 10 in
Weight : 192,000 lb empty / 477,000 lb max. take off
Ceiling : 47,900 ft
Speed :
@ high altitude : 1,324 km/h
/ 823 mph
@ low level (200ft) : 965
km/h / 600 mph
Range : More than 12,000 km / 7,455 miles
Engine : Two General Electric F110-GE-102
afterburning turbofan, 30,780 lb thrust each
Armament : Internal bays for up to 75,000 lb of
ordnance including conventional bombs, nuclear bombs, AGM-86 cruise missles, or
SRAMs.
B-1B Lancer - U.S.A Nuclear Forces
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