B-1 Lancer
Specifications
(B-1B) General
characteristics * Crew: 4 (aircraft commander, copilot,
offensive systems officer and defensive systems officer) * Length: 146 ft (44.5 m) * Wingspan: o Extended: 137 ft (41.8 m) o Swept: 79 ft (24.1 m) * Height: 34 ft (10.4 m) * Wing area: 1,950 ft² (181.2 m²) * Airfoil: NA69-190-2 * Empty weight: 192,000 lb (87,100 kg) * Loaded weight: 326,000 lb (148,000 kg) * Max
takeoff weight: 477,000 lb (216,400 kg) * Powerplant: 4× General Electric
F101-GE-102 augmented turbofans o Dry thrust: 14,600 lbf (64.9 kN)
each o Thrust with afterburner: 30,780 lbf
(136.92 kN) each * Fuel capacity, optional: 10,000 Performance * Maximum speed: Mach 1.25 (950 mph, 1,529
km/h) at altitude (Mach 0.92, 700 mph, 1,130 km/h at low level) * Range: 6,478 nmi (7,456 mi, 11,998 km) * Combat radius: 2,993 nmi (3,445 mi, 5,543
km) * Service ceiling 60,000 ft (18,000 m) * Wing loading: 167 lb/ft² (816 kg/m²) * Thrust/weight: 0.37 Units 13th Bomb Squadron  |
Armament * Hardpoints: six external hardpoints for
59,000 lb (27,000 kg) of ordnance (use for weapons currently restricted by START I treaty) and 3 internal bomb bays
for 75,000 lb (34,000 kg) of ordnance
to carry from: * Missiles: o 24× AGM-158 JASSM o 12× AGM-154 JSOW * Bombs: o 84× Mk-82 AIR inflatable retarder
general purpose bombs o 81× Mk-82 low drag general purpose
bombs o 84× Mk-62 Quickstrike sea mines o 8× Mk-65 naval mines o 30× CBU-87/89/CBU-97 Cluster Bomb
Units (CBU) o 30× CBU-103/104/105 WCMD o 24× GBU-31 JDAM GPS guided bombs o 15× GBU-38 JDAM GPS guided bombs
(Mk-82 general purpose warhead) o 24× Mk-84 general purpose bombs o 96× or 144× GBU-39 Small Diameter
Bomb GPS guided bombs o 16x B61 thermonuclear
variable-yield gravity bombs Avionics * 1× Westinghouse AN/APQ-164
forward-looking offensive passive phased-array radar * 1× Eaton AN/ALQ-161 radar warning and
defensive jamming equipment * 1× AN/ASQ-184 defensive management system * 1× Lockheed Martin Sniper XR targeting
pod(optional) |
