Crew 4
Dimensions
wing span, wings forward 55.7 metres
wing span with wings swept 35.6 metres
Length 54.1 metres
Height 13.1 metres
Weights
maximum take off weight 275 tons
normal combat load weight 9,000 tons
maximum combat load weight 40,000 tons
fuel weight 148,000 kg
Performance
operational flight range with normal combat load 14,000 km
operational flight range with maximum combat load 10,500 km
maximum flight speed at high altitude 2,000 km/h
maximum flight speed near ground 1,030 km/h
service ceiling 16,000 metres
concrete runway length 3,050 metres
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Primary Function: Long-range, multi-role, heavy bomber
Builder: Rockwell International, North American Aircraft
Operations Air Frame and Integration: Offensive avionics, Boeing Military Airplane; defensive avionics, AIL Division
Power Plant: Four General Electric F-101-GE-102 turbofan engine with afterburner
Thrust: 30,000-plus pounds (13,500-plus kilograms) with afterburner, per engine
Length: 146 feet (44.5 meters)
Wingspan: 137 feet (41.8 meters) extended forward,
79 feet (24.1 meters) swept aft
Height: 34 feet (10.4 meters)
Weight: Empty, approximately 190,000 pounds (86,183 kilograms)
Maximum Takeoff Weight: 477,000 pounds (214,650 kilograms)
Speed: 600+ mph (Mach .92) @ 500 feet
825 mph (Mach 1.25) @ 50,000 feet
Rotate and Takeoff Speeds: 210 Gross - 119 Rotate kts / 134 kts Takeoff
390 Gross - 168 kts Rotate / 183 kts Takeoff
Landing Speeds: 210 Gross - 145 kts
380 Gross - 195 kts
Range: 7,455 miles, unrefueled
3,444 miles with normal weapons load
Ceiling: 60,000 feet (18,000 meters)
Crew: Four (aircraft commander, pilot, offensive systems officer and defensive systems officer)
Armament:
NUCLEAR
CONVENTIONAL
84 Mk 62
84 MK82
30 CBU 87
30 CBU 89
30 CBU 97
12 Mk 65
PRECISION
30 WCMD
24 JDAM
12 GBU-27
12 AGM-154 JSOW
12 TSSAM
Date Deployed: June 1985
Unit Cost: $200-plus million per aircraft
Inventory: 100 total production
92 total current inventory
Active force, 51 PMAI (68 actual)
ANG, 18 PMAI (22 actual)
Reserve, 0
AFMC, 2 (Test)
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