Primary Function A-10 -- close air support, OA-10 - airborne forward air control Contractor Fairchild Republic Co. Power Plant Two General Electric TF34-GE-100 turbofans Thrust 9,065 pounds each engine Length 53 feet, 4 inches (16.16 meters) Height 14 feet, 8 inches (4.42 meters) Wingspan 57 feet, 6 inches (17.42 meters) Speed 420 miles per hour (Mach 0.56) Ceiling 45,000 feet (13,636 meters)  Maximum Takeoff  Weight 51,000 pounds (22,950 kilograms) Range 800 miles (695 nautical miles)

Contractors Boeing McDonnell Douglas Helicopter Systems (Mesa, AZ) General Electric (Lynn, MA) Martin Marietta (Orlando, FL) Propulsion Two T700-GE-701Cs Crew Two AH-64A  AH-64D Length 58.17 ft (17.73 m) 58.17 ft (17.73 m) Height 15.24 ft (4.64 m) 13.30 ft (4.05 m) Wing Span 17.15 ft (5.227 m) 17.15 ft (5.227 m) Primary Mission Gross Weight 15,075 lb (6838 kg) 11,800 pounds Empty 16,027 lb (7270 kg) Lot 1 Weight Hover In-Ground Effect (MRP) 15,895 ft (4845 m) Vertical Rate of Climb (MRP) 2,175 fpm (663 mpm)  Maximum Rate of Climb (IRP) 2,915 fpm (889 mpm)  Maximum Level Flight Speed 150 kt (279 kph) Cruise Speed (MCP) 150 kt (279 kph) Range 400 km - internal fuel 1,900 km - internal and external fuel Armament M230 30mm Gun 70mm (2.75 inch) Hydra-70 Folding-Fin Aerial Rockets AGM-114 Hellfire anti-tank missiles AGM-122 Sidearm anti-radar missile AIM-9 Sidewinder Air-to-Air missiles.  To save as wallpaper right click on photo and choose "Save As Background"

Function Carrier-based multi-role strike fighter Contractor Grumman Aerospace Corporation Unit Cost $38 million Propulsion F-14: two Pratt & Whitney TF-30P-414A turbofan engines with afterburners Length 61 feet 9 inches (18.6 meters) Height 16 feet (4.8 meters) Basic Weight approx 43,600 pounds Maximum Takeoff Weight 72,900 pounds (32,805 kg) Wingspan 64 feet (19 meters)  Ceiling Above 53,000 feet Max G 6.5 Speed 1,584 mph (Max Mach Number = 1.88 Cruise Mach Number = .72 Carrier Approach Speed = 125 kts Fuel 16, 200 lbs. Internal fuel 3, 800 lbs. External fuel Maximum range1,600 nm  Field takeoff distance 2,400 ft.  Crew Two: pilot and radar intercept officer.  To save as wallpaper right click on photo and choose "Save As Background"

Primary Function Tactical fighter.Tactical Bomber Contractor Boeing (McDonnell Aircraft and Missiles Systems) Boeing (McDonnell Aircraft and Missiles Systems) Power Plant Two Pratt & Whitney F100-PW-100 turbofan engines with afterburners, each rated at 25,000 pounds engine ( 11,250 kilograms)  Length 63 feet, 9 inches (19.43 meters). 63 ft 9 in (19.43 m) Height 18 feet, 8 inches (5.69 meters). 18 ft 5.5 in (5.63 m) Wingspan 42 feet, 10 inches (13.06 meters) 42ft 9.75 in (13.05 m)  Speed 1,875 mph (Mach 2.5-plus). 1,433 kt (1,650 mph; 2655 km/h) maximum level speed 'clean' at high altitude 495 kt (570 mph; 917 km/h) cruising speed at optimum altitude Ceiling 65,000 feet (19,697 meters). 60,000 ft (18290 m); Operating Empty Weight 31,700 lb (14379 kg) Maximum Takeoff  Weight 68,000 pounds (30,600 kilograms). 81,000 lb (36741 kg) fuel 13,123 lb (5952 kg) internal 21,645 lb (9818 kg) in two CFTs up to three 610-US gal (2309-liter~ drop tanks; Range 3,450 miles (3,000 nautical miles) ferry range with conformal fuel tanks and three external fuel tanks. 3,100 nm (3,570 miles; 5745 km) ferry range with CFTs and drop tanks 2,400 nm (2,765 miles; 4445 km) with drop tanks 1,000 nm (1,150 mi; 1,853 km)  To save as wallpaper right click on photo and choose "Save As Background"

F-16

Primary Function Multirole fighter  Builder Lockheed Martin Corp. Power Plant  F-16C/D: one Pratt and Whitney F100-PW-200/220/229 or one General Electric F110-GE-100/129  Thrust F-16C/D, 27,000 pounds(12,150 kilograms) Length 49 feet, 5 inches (14.8 meters) Height 16 feet (4.8 meters) Wingspan 32 feet, 8 inches (9.8 meters) Speed 1,500 mph (Mach 2 at altitude) Ceiling Above 50,000 feet (15 kilometers) Maximum Takeoff  Weight 37,500 pounds (16,875 kilograms) Combat Radius [F-16C]

Contractor Boeing [McDonnell Douglas Aerospace] and Northrop Grumman (Airframe), General Electric (Engines), and Hughes (Radar) F/A-18C/D Hornet F/A-18E/F Super Hornet Power Plant Two F404-GE-402 afterburning engines, each in the 18,000 pound thrust class, which results in a combat thrust-to-weight ratio greater than 1-to-1. Combat Radius is greater than 500 nautical miles. Twin F414-GE-400 engines, each in the 22,000 pound thrust class. The F/A-18C and F/A-18E are single seat aircraft. The D and F models are flown by two crew members. The aft seat in the D and F may be configured with a stick and throttle for the training environment (or without when crewed with a  Weapons System Officer). Performance F/A-18C maximum speed at level flight in altitudes of 36,089 ft. Mach 1.7 F/A-18E maximum speed at level flight in altitudes of 36,089 ft. Mach 1.6 Armament F/A-18C/D can carry up to 13,700 pounds of external ordnance. Weapon :   M61 Vulcan 6-barrel rotary cannon with 520 rounds of 20mm ammunition is internally mounted in the nose. To save as wallpaper right click on photo and choose "Save As Background"

Official Nickname Raptor  Function Air superiority fighter  Contractors Lockheed Martin Aeronautical Systems: F-22 program management, the integrated forebody (nose section) and forward fuselage (including the cockpit and inlets), leading edges of the wings, the fins and stabilators, flaps, ailerons, landing gear and final assembly of the aircraft. Lockheed Martin Tactical Aircraft Systems: Center fuselage, stores management, integrated navigation and electronic warfare systems (INEWS), the communications, navigation, and identification (CNI) system, and the weapon support system.  Boeing: wings, aft fuselage (including the structures necessary for engine and nozzle installation), radar system development and testing, avionics integration, the training system, and flight-test development and management. Pratt & Whitney: F119-PW-100 engines that power the Raptor. Major Subcontractors Approximately 240 firms in 37 states are considered major subcontractors  More than 1,150 firms in 46 states and Puerto Rico, along with firms in seven international countries make up the F-22/F119 subcontractor team. Propulsion two Pratt & Whitney F119-PW-100 engines Thrust 35,000 lbst  Length 62.08 feet, 18.90 meters  Height 16.67 feet, 5.08 meters  Wingspan 44.5 feet, 13.56 meters  Wing Area 840 square feet  Horizontal Tailspan 29 feet, 8.84 meters  Maximum Takeoff  Weight  x   Ceiling x   Speed Mach 1.8 (supercruise: Mach 1.5)  Crew one pilot  Armament Two AIM-9 Sidewinders  six AIM-120C Advanced Medium-Range Air-to-Air Missiles (AMRAAM)  one 20mm Gatling gun  two 1,000-pound Joint Direct Attack Munitions (JDAM)  To save as wallpaper right click on photo and choose "Save As Background"

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  2 GBU-10 Paveway II  2 GBU-12 Paveway II  2 GBU-27 Paveway III  2 BLU 109  2 WCMD  2 Mark 61 Crew One  To save as wallpaper right click on photo and choose "Save As Background"

Origin: Germany, Italy, Spain, UK  Type: Attack Fighter Crew: 1  Max Speed: 2,125 km/h - 1,321 mph  Take-off Distance: 500 meters - 1,640 feet  Dimensions: Wingspan: 10.50 meters - 34 feet, 5.5 inches  Length: 14.50 meters - 47 feet, 7 inches  Height 6.40 meters - 21 feet  Max weight: 21,000 kilograms - 46,297 pounds  Power Plant: two 90 kN (20,250 lb st) Eurojet EJ200 afterburning turbofans Armament: One Mauser Mk27 27mm cannon; up to 6,500 kilograms (14,330 pounds) of ordinance can include: AIM-120 AMRAAMs, Aspide AAMs, short-range AAMs, various air-to-surface weapons, three auxillary fuel tanks.

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 Payload: 40,000 pounds (18,000 kilograms) Crew: Two pilots  To save as wallpaper right click on photo and choose "Save As Background"

Primary Function: Heavy bomber Contractor: Boeing Military Airplane Co. Power Plant: Eight Pratt & Whitney engines TF33-P-3/103 turbofan Thrust: Each engine up to 17,000 pounds (7,650 kilograms) Length: 159 feet, 4 inches (48.5 meters) Height: 40 feet, 8 inches (12.4 meters) Wingspan: 185 feet (56.4 meters) Speed: 650 miles per hour (Mach 0.86) Ceiling: 50,000 feet (15,151.5 meters) Weight: Approximately 185,000 pounds empty (83,250 kilograms) Maximum Takeoff Weight: 488,000 pounds (219,600 kilograms) Range: Unrefueled 8,800 miles (7,652 nautical miles) Armament: Approximately 70,000 pounds (31,500 kilograms) mixed ordnance -- bombs, mines and missiles. NOTE: The B-52 can carry 27 internal weapons. Authoritative sources diverge as to maximum munition loads, with some suggesting as many as 51 smaller munitions and 30 larger munitions, while others suggest maximum loads of 45 and 24, respectively. The Heavy Stores Adaptor Beam [HSAB] external pylon can carry only 9 weapons which limits the total carry to 45 (18 external). The AGM-28 pylon could carry lighter weapons like the MK-82 and can carry 12 weapons on each pylon, for a total of 24 external weapons, for a the total of 51. However, the AGM-28 pylon is no longer used, so the B-52 currently carries on HSABs, limiting the external load to 18 bombs, or a total of 45 bombs.  To save as wallpaper right click on photo and choose "Save As Background"

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