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Air Power Series>1:72 die-cast display model>F-22>HA2827

F-22 Raptor 91-4007, 412 TW, Edwards AFB
HA2827
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.
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.