The B-1 is a long-range strategic bomber with a distinctive streamlined shape. It was originally designed to deliver nuclear weapons to targets in defended Soviet airspace, but can carry a variety of conventional arms as well. |
B1-B Lancer
Primary function: Long-range, multi-role, heavy bomber Builder: Boeing, North America (formerly Rockwell) Speed: 900+ mph (mach 1.2) Armament: Short-range attack missiles, bombs and cruise missiles Crew: Four (aircraft commander, copilot, offensive systems officer and defensive systems officer) Power plant: Four General Electric F-101-GE-102 turbofan engine with afterburner Thrust: 30,000-plus pounds 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 (216,634 kilograms) Range: Intercontinental, unrefueled Ceiling: More than 30,000 feet (9,144 meters) Date Deployed: June 1985 Unit Cost: $283.1 million (fiscal 98 constant dollars) Inventory: Active force, 51 primary mission aircraft inventory (72 actual), 2 (test); ANG, 18 PMAI (20 actual); Reserve, 0
Photos: photo1 photo2 photo3 photo4
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Armament:
Three internal weapons bays can accommodate up to 84 Mk-82 general purpose bombs
or Mk-62 naval mines, 30 CBU-87/89 cluster munitions or CBU-97 Sensor Fused
Weapons and up to 24 GBU-31 JDAM GPS guided bombs or Mk-84 general purpose bombs
http://www.af.mil/news/factsheets/B_1B_Lancer.html
http://www.fas.org/nuke/guide/usa/bomber/b-1b.htm
http://www.fas.org/nuke/guide/usa/bomber/b-1b_gallery.htm (photos)
The B-2 Spirit is a multi-role bomber capable of delivering both conventional and nuclear munitions anywhere on the globe. Its "stealth" characteristics blend low-observable technologies with high aerodynamic efficiency and large payload, providing greater freedom of action at high altitudes. This increases its unrefueled range to approximately 6,000 nautical miles. |
B-2 Spirit
Primary function: Multirole heavy bomber Speed: High subsonic
Armament: Conventional or nuclear weapons Prime Contractor: Northrop Grumman Corp. 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) Ceiling: 50,000 feet (15,152 meters) Takeoff Weight (Typical): 336,500 pounds (152,635 kilograms) Range: Intercontinental, unrefueled 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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Armament: |
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NUCLEAR |
CONVENTIONAL |
PRECISION |
http://www.airforce-technology.com/projects/b2/index.html
http://www.globalsecurity.org/wmd/systems/b-2.htm
http://www.globalsecurity.org/wmd/systems/b-2-history.htm
http://www.globalsecurity.org/wmd/systems/b-2-ref.htm (references)
http://www.globalsecurity.org/wmd/systems/b-2_gallery.htm (photos)
http://www.aerotechnews.com/phtoarc/webphot/b1b/b1b7jpg.html (photos)
http://www.af.mil/news/factsheets/B_2_Spirit.html
F-117 Nighthawk Primary function: Fighter/attack Speed: sub mach 1 Armament: Two each of: 2
MK84 2000-pound
Crew: one
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Specifications |
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Primary Function |
Fighter/attack |
Contractor |
Lockheed Aeronautical Systems Co. |
Power Plant |
Two General Electric F404 engines |
Length |
65 feet, 11 inches (20.3 meters) |
Height |
12 feet, 5 inches (3.8 meters) |
Weight |
52,500 pounds (23,625 kilograms) |
Wingspan |
43 feet, 4 inches (13.3 meters) |
Speed |
High subsonic |
Range |
Unlimited with air refueling |
Armament |
Internal weapons carriage Two each of: 2
MK84 2000-pound |
Unit Cost
$FY98 |
$122 million |
Crew |
One |
Date Deployed |
1982 |
Inventory |
Active force, 54; ANG, 0; Reserve, 0 |
PMAI
Only combat-coded aircraft and not development/ test, attrition reserve, depot maintenance, or training aircraft. |
36 aircraft |
VRML 3-D Model | |
F-117A Nighthawk VRML by Soji Yamakawa |
F-117 |
F-117 Web Sites:
http://www.fas.org/man/dod-101/sys/ac/f-117.htm (photos)
http://www.jetplanes.co.uk/f117.html
http://www.holloman.af.mil/photos/117pho.html (photos)
http://www.geocities.com/CapeCanaveral/Hangar/3314/f117.html
http://www.airforce-technology.com/projects/f117/
http://www.af.mil/news/factsheets/F_117A_Nighthawk.html
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F-22 Raptor
Primary function: Fighter/attack Speed: high supersonic Crew: Replaces: F4, F111, F15 Wingspan: 44 feet 6 inches Length: 62 feet 1 inch Height: 16 feet 5 inches Powerplant: two F119-100 from Pratt and Whitney Thrust: 156 kN Auxiliary power unit: G250, 335 kW Allied Signal Aerospace Weapons:
M61A2 Vulcan Cannon
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http://www.f-22raptor.com/index_ie.htm
http://www.codeonemagazine.com/f22/index.html
http://www.af.mil/lib/airpower
http://www.boeing.com/defense-space/military/f22/f22photos.htm
http://www.airforce-technology.com/projects/f22/index.html
Stealth Web Sites:
http://www.af.mil/news/Feb1999/n19990216_990243.html