F-117A NIGHTHAWK
The F-117A Nighthawk Stealth Fighter Attack Aircraft was developed by Lockheed Martin after work on stealth technology and the predecessor test demonstrator aircraft, Have Blue, was carried out in secret from 1975. Development of the F-117A began in 1978 and it was first flown in 1981, but it was not until 1988 that its existence was publicly announced. The Nighthawk is the world's first operational stealth aircraft. The US Air Force has 59 Nighthawks.

The F-117A aircraft is also known as the Frisbee and the Wobblin' Goblin. The mission of the aircraft is to penetrate dense threat environments and attack high value targets with high accuracy. Nighthawk was in operational service during Operation Desert Storm.

DESIGN

The surfaces and edge profiles are optimised to reflect hostile radar into narrow beam signals directed away from the enemy radar detector. All the doors and opening panels on the aircraft have saw-toothed forward and trailing edges to reflect radar. The aircraft is mainly constructed of aluminium with titanium for areas of the engine and exhaust systems. The outer surface of the aircraft is coated with a radar absorbent material (RAM). The radar cross-section of the F-117 has been estimated at between 10 and 100 square cm.

The F-117A has four elevons on the inboard and outboard trailing edge of the wing. The V-shaped tail which controls the yaw of the aircraft acts as a flying tail which means that the whole surface acts as a control surface. The elevons do not act as flaps to reduce the rate of descent for touchdown so the landing speed of the F-117A is high at about 180 or 190 miles per hour and a drag parachute is used.

COCKPIT

The cockpit has a Kaiser Electronics head up display (HUD) and the flight deck is equipped with a large video monitor which displays the infrared imagery from the aircraft's onboard sensors. The cockpit has a full colour moving map developed by the Harris Corporation. The fly-by-wire system is supplied by BAE SYSTEMS Astronics.

WEAPONS

The aircraft can carry a range of tactical fighter ordnance in the weapons bay, including BLU-109B low level laser guided bomb, GBU-10 and GBU-27 laser guided bomb units, Raytheon AGM-65 Maverick and Raytheon AGM-88 HARM air-to-surface missiles.

SENSORS

For stealth, the F-117A does not rely on radar for navigation or targeting. For navigation and weapon aiming the aircraft is equipped with a forward-looking infrared (FLIR) and a downward looking infrared (DLIR) with laser designator, supplied by Raytheon. The aircraft uses a Honeywell inertial navigation system.

The aircraft has multi-channel pitot static tubes installed in the nose. Multiple ports along the length of the tubes provide differential pressure readings. The flight control computers compare these in order to provide the aircraft's flight data.

FLIGHT MANAGEMENT

Before flight, mission data is downloaded on to the IBM AP-102 mission control computer which integrates it with the navigation and flight controls to provide a fully automated flight management system.

After take-off, the pilot can hand over flight control to the mission program until within visual range of the mission's first target. The pilot then resumes control of the aircraft for weapon delivery. The aircraft is equipped with an infrared acquisition and designation system (IRADS), which is integrated with the weapon delivery system. The pilot is presented with a view of the target on the head-up display, first from the FLIR and then from the DLIR. The weapon delivery and impact is recorded on the aircraft's internally mounted video system which provides real time damage assessment.

ENGINES

The F-117A is powered by two low bypass F404-GE-F1D2 turbofan engines from General Electric. The rectangular air intakes on both sides of the fuselage are covered by gratings which are coated with radar absorbent material.

The wide and flat structure of the engine exhaust area reduces the infrared and radar detectability of the aft section of the engine. The two large tail fins slant slightly outwards to provide an obstruction to the infrared and radar returns from the engine exhaust area.
F-117A NIGHTHAWK - SPECIFICATION
Crew  one 
Dimensions    
Angle of sweep of delta wing  67 degrees 30 minutes 
Estimated wingspan x length x height  43ft x 66ft x 12ft 6in 
Weights    
Maximum gross weight  52,500 pounds 
Weapons    
Armament in internal weapon bays  BLU-109B low level laser guided bomb 
   GBU-10 
   GBU-27 laser guided bomb units, 
   AGM-65 Maverick 
   AGM-88 HARM 
   BDU-33 practice bombs 
Performance    
Speed  high subsonic 
Range  unlimited with air refuelling 
USAF production  59 aircraft
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