Mission
The F-22 Raptor is the Air Force's newest fighter aircraft. Its
combination of stealth, supercruise, maneuverability, and integrated
avionics, coupled with improved supportability, represents an
exponential leap in warfighting capabilities. The Raptor performs both
air-to-air and air-to-ground missions allowing full realization of
operational concepts vital to the 21st century Air Force.
The F-22, a critical component of the Global Strike Task Force, is
designed to project air dominance, rapidly and at great distances and
defeat threats attempting to deny access to our nation's Air Force,
Army, Navy and Marine Corps. The F-22 cannot be matched by any known or
projected fighter aircraft.
Features
A combination of sensor capability, integrated avionics, situational
awareness, and weapons provides first-kill opportunity against threats.
The F-22 possesses a sophisticated sensor suite allowing the pilot to
track, identify, shoot and kill air-to-air threats before being
detected. Significant advances in cockpit design and sensor fusion
improve the pilot's situational awareness. In the air-to-air
configuration the Raptor carries six AIM-120 AMRAAMs and two AIM-9
Sidewinders.
The F-22 has a significant capability to attack surface targets. In the
air-to-ground configuration the aircraft can carry two 1,000-pound
GBU-32 Joint Direct Attack Munitions internally and will use on-board
avionics for navigation and weapons delivery support. In the future
air-to-ground capability will be enhanced with the addition of an
upgraded radar and up to eight small diameter bombs. The Raptor will
also carry two AIM-120s and two AIM-9s in the air-to-ground
configuration.
Advances in low-observable technologies provide significantly improved
survivability and lethality against air-to-air and surface-to-air
threats. The F-22 brings stealth into the day, enabling it not only to
protect itself but other assets.
The F-22 engines produce more thrust than any current fighter engine.
The combination of sleek aerodynamic design and increased thrust allows
the F-22 to cruise at supersonic airspeeds (greater than 1.5 Mach)
without using afterburner -- a characteristic known as supercruise.
Supercruise greatly expands the F-22 's operating envelope in both speed
and range over current fighters, which must use fuel-consuming
afterburner to operate at supersonic speeds.
The sophisticated F-22 aerodesign, advanced flight controls, thrust
vectoring, and high thrust-to-weight ratio provide the capability to
outmaneuver all current and projected aircraft. The F-22 design has been
extensively tested and refined aerodynamically during the development
process.
The F-22's characteristics provide a synergistic effect ensuring F-22A
lethality against all advanced air threats. The combination of stealth,
integrated avionics and supercruise drastically shrinks surface-to-air
missile engagement envelopes and minimizes enemy capabilities to track
and engage the F-22 . The combination of reduced observability and
supercruise accentuates the advantage of surprise in a tactical
environment.
The F-22 will have better reliability and maintainability than any
fighter aircraft in history. Increased F-22 reliability and
maintainability pays off in less manpower required to fix the aircraft
and the ability to operate more efficiently.
Background
The Advanced Tactical Fighter entered the Demonstration and Validation
phase in 1986. The prototype aircraft (YF-22 and YF-23) both completed
their first flights in late 1990. Ultimately the YF-22 was selected as
best of the two and the engineering and manufacturing development effort
began in 1991 with development contracts to Lockheed/Boeing (airframe)
and Pratt & Whitney (engines). EMD included extensive subsystem and
system testing as well as flight testing with nine aircraft at Edwards
Air Force Base, Calif. The first EMD flight was in 1997 and at the
completion of its flight test life this aircraft was used for live-fire
testing.
The program received approval to enter low rate initial production in
2001. Initial operational and test evaluation by the Air Force
Operational Test and Evaluation Center was successfully completed in
2004. Based on maturity of design and other factors the program received
approval for full rate production in 2005. Air Education and Training
Command, Air Combat Command and Pacific Air Forces are the primary Air
Force organizations flying the F-22. The aircraft designation was the
F/A-22 for a short time before being renamed F-22A in December 2005.
General Characteristics
Primary Function: Air dominance, multi-role fighter
Contractor: Lockheed-Martin, Boeing
Power Plant: Two Pratt & Whitney F119-PW-100 turbofan engines with afterburners and two-dimensional thrust vectoring nozzles.
Thrust: 35,000-pound class (each engine)
Wingspan: 44 feet, 6 inches (13.6 meters)
Length: 62 feet, 1 inch (18.9 meters)
Height: 16 feet, 8 inches (5.1 meters)
Weight: 43,340 pounds (19,700 kilograms)
Maximum Takeoff Weight: 83,500 pounds (38,000 kilograms)
Fuel Capacity: Internal: 18,000 pounds (8,200 kilograms); with 2 external wing fuel tanks: 26,000 pounds (11,900 kilograms)
Payload: Same as armament air-to-air or air-to-ground loadouts; with or without 2 external wing fuel tanks.
Speed: Mach 2 class with supercruise capability
Range: More than 1,850 miles ferry range with 2 external wing fuel tanks (1,600 nautical miles)
Ceiling: Above 50,000 feet (15 kilometers)
Armament: One M61A2 20-millimeter cannon with 480
rounds, internal side weapon bays carriage of two AIM-9 infrared (heat
seeking) air-to-air missiles and internal main weapon bays carriage of
six AIM-120 radar-guided air-to-air missiles (air-to-air loadout) or two
1,000-pound GBU-32 JDAMs and two AIM-120 radar-guided air-to-air
missiles (air-to-ground loadout)
Crew: One
Unit Cost: $143 million
Initial operating capability: December 2005
Inventory: Total force, 183
Point of Contact
Air Combat Command, Public Affairs Office; 130 Andrews St., Suite 202; Langley AFB, VA 23665-1987; DSN 574-5007 or 757-764-5007; e-mail: accpa.operations@langley.af.mil
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