Overview
The Rockwell B-1B Lancer is a variable-sweep wing strategic bomber developed for the United States Air Force. Originally conceived during the Cold War, it evolved into a platform optimized for conventional strike missions. The aircraft combines high payload capacity with intercontinental range.
Live Fleet Activity (B1)
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Specifications
Units
- Engine
- 4 × General Electric F101-GE-102
- Engine type
- Turbofan
- Thrust
- 4 × 30,780 lbf · 137 kN
- Avionics
- AN/APQ-164, AN/ALQ-161, AN/ASQ-184
- Wing tips
- No winglets
- Seats
- 4
- Crew
- —
- Cabin width
- —
- Cabin height
- —
- Cabin length
- —
- Exterior length
- 147 ft 0 in · 44.80 m
- Tail height
- 34 ft 1 in · 10.40 m
- Fuselage diameter
- 8 ft 6 in · 2.60 m
- Wing span
- 137 ft 2 in · 41.80 m
- Baggage volume
- —
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 477,500 lb · 216,500 kg
- Max landing weight
- —
- Max payload
- 75,000 lb · 34,000 kg
- Fuel capacity
- 39,600 gal · 149,900 L · 119,900 kg (Jet A)
- Max cruise speed
- 825 kt · 949 mph · 1,528 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- 250 kt · 288 mph · 463 km/h
- Range
- 6,485 nm · 7,460 mi · 12,010 km
- Fuel burn
- 0.16 nm/gal · 0.08 km/L
- Ceiling
- 60,000 ft · 18,300 m
- Rate of climb
- 6,000 ft/min · 30 m/s
- Takeoff distance
- 1,970 ft · 600 m
- Landing distance
- 1,380 ft · 420 m
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