Air Power Series>1:72 die-cast display model>F-22>HA2811B

General Background

The USAF developed a requirement for a new air superiority fighter to replace the F-15 Eagle. Two proposals were submitted with the Lockheed Martin F-22 Raptor being selected as the new Advanced Tactical Fighter (ATF). The aircraft is constructed using 39% titanium, 24% composite material, 16% aluminum and 1% thermoplastic by weight. All these components contribute to the F-22 being a light weight, extremely maneuverable, extremely fast aircraft that uses stealth technology. The F-22 is also capable of ground attack, electronic warfare and signals intelligence.

The Aircraft

In 1986 Northrop and Lockheed Martin were each awarded a demonstration and concept validation contract. The Lockheed YF-22 won over Northrop’s YF-23. The YF-22 first flew on September 29, 1990 with the flight of the first production F-22 “Raptor” taking place on September 7, 1997. This aircraft was number 91-4001 with a serial of 91-001 and named “Spirit of America”. In October 1997 91-001 went to Edwards AFB in California for testing. What started with 91-001 will end in 2013 when the last planned 438th F-22 is delivered.

Specifications :

First flight:	September 7, 1997
Planned Production:	750 aircraft initial program objective
Altered plan in 1990:	648 aircraft
Altered plan in 1994:	442 aircraft
In 1997 Department of Defense report:	339 aircraft
In 2006 the Pentagon wanted -183 aircraft:	2008 approval for 4 additional aircraft bringing the total to 187
Number built as of August 2009:	145
Role:	Air superiority fighter
Crew:	(1) pilot
Performance
Engines:	(2) Pratt & Whitney F119-PW-100 engines producing 35,000 lbst of thrust
Speed:	Mach 1.8 (super cruise: Mach 1.5)
G Limit:	+9 G
Ceiling:	60,000 ft (18,290 m)
	The F-22 and other fighters can reach this altitude, but only the F-22 can perform tactical maneuvers at this level.
Dimensions
Length:	62.08 ft (18.90 m)
Height:	16.67 ft (5.08 m)
Wingspan:	44.5 ft (13.56 m)
Wing Area:	840 sq ft (78.04 sq m)
Horizontal Tail-span:	29 ft (8.84 m)
Weights
Empty Weight:	31,670 lb (14,365 kg)
Maximum Takeoff Weight:	60,000 lb (27,000 kg)
Armament:
Internal:	(1) 20mm Cannon
	(4) AIM-9 Sidewinders (side weapon bays)
	(4) AIM-120A AMRAAM (internal ventral bay)
	(6) AIM-120Cs (internal ventral bay)
	(6) GBU-32 JDAM PGMs (internal ventral bay)
	(8) GBU-39 Small Diameter Bombs (250lbs ea)
External:	(4) under-wing hard-points with a maximum of 5,000lbs (2,270kg) of mission-specific weaponry or fuel drop-tanks.