From Wikipedia, the free encyclopedia
Type Stealth attack aircraft
Manufacturer Lockheed Skunk Works Lockheed Martin
Maiden flight 18 June 1981 Retired 21 April 2008 (planned)
Number built 64 (5 YF-117A, 59 F-117A)
The
The Air Force will retire the F-117 on 21 April 2008, primarily due to the purchasing and eventual deployment of the more effective F-22 Raptor and F-35 Lightning II.
Design
About the size of an F-15C Eagle, the single-seat F-117A is powered by two non-afterburning General Electric F404 turbofan engines, and has quadruple-redundant fly-by-wire flight controls. It is air refuelable. In order to lower development costs, the avionics, fly-by-wire systems, and other parts are derived from the F-16 Fighting Falcon, F/A-18 Hornet and F-15E Strike Eagle. The parts were originally described as spares on budgets for these aircraft, to keep the F-117 project secret.
Among the penalties for stealth are lower engine power thrust, due to losses in the inlet and outlet, a very low wing aspect ratio, and a high sweep angle (50°) needed to deflect incoming radar waves to the sides.
The F-117A is equipped with sophisticated navigation and attack systems integrated into a digital avionics suite. It carries no radar, which lowers emissions and cross-section. It navigates primarily by GPS and high-accuracy inertial navigation. Missions are coordinated by an automated planning system that can automatically perform all aspects of a strike mission, including weapons release. Targets are acquired by a thermal imaging infrared system, slaved to a laser that finds the range and designates targets for laser-guided bombs.
The F-117A's split internal bay can carry 5,000 lb (2,300 kg) of ordnance. Typical weapons are a pair of GBU-10, GBU-12, or GBU-27 laser-guided bombs, two BLU-109 penetration bombs, or two Joint Direct Attack Munitions (JDAMs), a GPS/INS guided stand-off bomb.
General characteristics
Crew: 1
Length: 69 ft 9 in (20.08 m)
Wingspan: 43 ft 4 in (13.20 m)
Height: 12 ft 9.5 in (3.78 m)
Wing area: 780 ft² (73 m²)
Empty weight: 29,500 lb (13,380 kg)
Loaded weight: 52,500 lb (23,800 kg)
Powerplant: 2× General Electric F404-F1D2 turbofans, 10,600 lbf (48.0 kN) each
Maximum speed: Mach 0.92 (617 mph, 993 km/h)
Cruise speed: Mach 0.92
Range: 930 NM[42] (1720 km)
Service ceiling 69,000 ft (20,000 m)
Wing loading: 65 lb/ft² (330 kg/m²)
Thrust/weight: 0.40
Armament
2× internal weapons bays with one hardpoint each (total of two weapons) equipped to carry:
Bombs:
BLU-109 hardened penetrator
GBU-10 Paveway II laser-guided bomb
GBU-12 Paveway II laser-guided bomb
GBU-27 Paveway III laser-guided bomb
JDAM INS/GPS guided munition
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