* Specifications *

Primary function: Multi-role heavy bomber.

Prime Contractor: Northrop Grumman Corp.

Contractor Team: Boeing Military Airplanes Co.,
General Electric Aircraft Engine Group
Hughes Training Inc., Link Division

Power Plant/Manufacturer: Four General Electric F-118-GE-100 engines

Thrust: 17,300 pounds each engine (7,847 kilograms)

Length: 69 feet (20.9 meters)

Height: 17 feet (5.1 meters)

Wingspan: 172 feet (52.12 meters)

Speed: High subsonic

Ceiling: 50,000 feet (15,152 meters)

Takeoff Weight (Typical): 336,500 pounds (152,635 kilograms)

Range: Intercontinental, unrefueled

Armament:

1.NUCLEAR

16 B61
16 B83
16 AGM-129 ACM
16 AGM-131 SRAM 2

2.CONVENTIONAL

80 MK82 [500lb]
16 MK84 [2000lb]
34-36 CBU87
34-36 CBU89
34-36 CBU97

3.PRECISION

80 GBU-30 JDAM [500lb]
16 GBU-32 JDAM [2000lb]
8 GBU 27
8 EGBU 28
8 GBU 36
8 GBU 37
8-16 AGM-154 JSOW
8-16 AGM-137 TSSAM

Payload: 40,000 pounds (18,000 kilograms)

Crew: Two pilots

Unit cost: Approximately $2.1 billion [average]

Date Deployed: December 1993

Inventory: Active force: 21 (planned operational aircraft); ANG: 0; Reserve: 0

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