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Northrop Grumman B-2 Spirit Intercontinental Strategic Bomber |
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DESCRIPTION:
The prototype B-2 stealth bomber emerged in 1988 after a decade of top secret research by the US Air Force. The B-2 design made great strides over previous attempts at stealth aircraft, such as the B-1B and F-117, thanks to a more refined understanding of radar wave reflection and its aerodynamic flying wing shape. The contoured wing shape of the B-2 Spirit contains the crew compartment, payload bays, and engines, thus hiding the most radar reflective components within its interior. In addition to being covered in radar absorbant materials (RAM), all of the lines of the B-2 are parallel to each other to scatter radar waves away from their point of origin (see 3-view below). Also, the engine exhaust is vented through a long trough covered with heat-absorbing materials to reduce the infrared heat signature of the B-2. The Air Force originally planned to acquire 133 stealth bombers but have since cut that number to a mere 21 active duty aircraft. Though originally designed as a nuclear strike platform, the B-2 has also been equipped to carry conventional weapons like JDAM. The B-2 has made extensive use of its new conventional strike role during recent conflicts in Kosovo, Afghanistan, and Iraq.
Last modified 29 November 2005
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| HISTORY: | |
| First Flight | 17 July 1989 |
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Service Entry
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April 1997
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CREW:
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two: pilot, co-pilot/mission commander
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ESTIMATED COST:
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$1.157 billion [1998$]
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| AIRFOIL SECTIONS: | |
| Wing Root | unknown |
| Wing Tip |
unknown
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| DIMENSIONS: | |
| Length | 69.00 ft (21.03 m) |
| Wingspan | 172.00 ft (52.43 m) |
| Height | 17.00 ft (5.18 m) |
| Wing Area | 5,000 ft2 (465.5 m2) |
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Canard Area
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not applicable
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| WEIGHTS: | |
| Empty | 150,000 to 160,000 lb (68,040 to 72,575 kg) |
| Normal Takeoff | 336,500 lb (152,635 kg) |
| Max Takeoff | 376,000 lb (170,550 kg) |
| Fuel Capacity |
internal: 200,000 lb (90,720 kg) external: none |
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Max Payload
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40,000 lb (18,145 kg)
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| PROPULSION: | |
| Powerplant | four General Electric F118-110 turbofans |
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Thrust
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76,000 lb (338 kN)
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| PERFORMANCE: | |
| Max Level Speed |
at altitude: 530 mph (850 km/h) at 40,000 ft (12,190 m), Mach 0.8 at sea level: 485 mph (780 km/h), Mach 0.65 cruise speed: 515 mph (830 km/h) at 37,000 ft (11,275 m), Mach 0.78 |
| Initial Climb Rate | 3,000 ft (915 m) / min |
| Service Ceiling | 50,000 ft (15,240 m) |
| Range |
typical: 6,000 nm (11,110 km) w/1 aerial refueling: 10,000 nm (18,520 km) |
| g-Limits |
+2.0
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| ARMAMENT: | |
| Gun | none |
| Stations | two internal bomb bays |
| Air-to-Surface Missile | up to 16 AGM-69 SRAM II, up to 16 AGM-129 ACM, AGM-154 JSOW |
| Bomb | up to 16 B61/B83 nuclear bombs, up to 80 Mk 82 500-lb GP, up to 16 Mk 84 2,000-lb GP, up to 36 M117 750-lb GP, up to 16 GBU-31 JDAM, up to 16 GBU-36, up to 8 GBU-37 (GAM-113), up to 36 CBU-87/89/97/98 cluster |
| Other |
up to 80 Mk 36 or Mk 62 500-lb sea mines
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| KNOWN VARIANTS: | |
| B-2A |
Original bomber operating from Whitman AFB, Missiouri; 22 built
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| KNOWN COMBAT RECORD: |
Kosovo - Operation Allied Force (USAF, 1999) Afghanistan - Operation Enduring Freedom (USAF, 2001) Iraq - Operation Iraqi Freedom (USAF, 2003) |
| KNOWN OPERATORS: |
United States (US Air Force)
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3-VIEW SCHEMATIC:
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SOURCES:
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