The first generation advanced bomber B-1B Lancer still carrying on service
- 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
- Exterior length:
- 146 ft 12 in · 44.80 m
- Tail height:
- 34 ft 1 in · 10.40 m
- Fuselage diameter:
- 8 ft 6 in · 2.60 m
- Wing span / rotor:
- 137 ft 2 in · 41.80 m
- Max takeoff weight:
-
477,500 lb
·
216,500 kg
- Max Payload:
-
75,000 lb
·
34,000 kg
- Fuel capacity:
-
39,600 gal
·
149,900 L
·
119,900 kg
(Jet A)
Cockpit of the B 1 Lancer
Rockwell B-1B Lancer ‘86-111 / EL'
Rockwell B-1B Lancer '85-0090'
Rockwell B-1B Lancer ‘85 066 / EL-28BW'
Rockwell B-1B Lancer ‘85-079 / EL'
Rockwell B-1B Lancer ‘85-072 / EL.
USAF Rockwell B-1B Lancer
Rockwell B-1B Lancer '85-073'
USAF Rockwell B-1B Lancer '85-0090'
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Blog Mentions
Blog posts that mention the Rockwell B-1B Lancer:
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