Lockheed Martin F-22A Raptor
| GENERAL DATA | |||
| Type |
Stealth air superiority fighter
|
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| Manufacturer(s) | Lockheed Martin
Aeronautics - Boeing Defense, Space & Security |
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| Prototype first flight | 7 September 1997 |
Introduction | 15 December 2005 |
| Produced | 1996–2011 |
Number built | 195: 8 test and 187 operational aircraft |
| Status | In service |
Crew | 1 |
| Variants | |||
| YF-22A | pre-production technology demonstrator for ATF demonstration/validation phase; two were built. | ||
| F-22A | single-seat production version, was designated F/A-22A in early 2000s. | ||
| F-22B | planned two-seat variant, canceled in 1996 to save development costs. | ||
| Naval F-22 Variant | a planned carrier-borne variant of the F-22 with variable-sweep
wings for the U.S. Navy's Navy Advanced Tactical Fighter (NATF) program
to replace the F-14 Tomcat. Program was canceled in 1993. |
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| DIMENSIONS | |||
| Length | 18.92 m |
Empty Weight | 19700 kg |
| Wingspan | 13.56 m |
Loaded Weight | 29410 kg |
| Height | 5.08 m |
Max takeoff weight | 38000 kg |
| Wing area | 78.04 m² |
Wing loading | 377 kg/m² |
| ARMAMENT | |||
| Guns | 1× 20 mm (0.787 in) M61A2
Vulcan rotary cannon |
Ammunition Carried |
480 |
| Hardpoints | 4× under-wing pylon stations
can be fitted to carry weapons (or drop tanks), each with a capacity
of 2270 kg
|
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| Air-to-air mission loadout | 6× AIM-120 AMRAAM, 2×
AIM-9 Sidewinder |
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| Air-to-ground mission loadout | 2× 450 kg JDAM or 8×
110 kg GBU-39 Small Diameter Bombs, 2× AIM-120 AMRAAM, 2×
AIM-9 Sidewinder |
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| POWERPLANT | |||
| Engine | 2 ×
Pratt & Whitney F119-PW-100 augmented turbofans
|
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| Dry thrust | 116 kN each |
Thrust with afterburner | 156 kN each |
| Thrust/weight | 1.08 (1.25 with loaded
weight
and 50% internal fuel) |
Fuel Capacity | 8200 kg internally, or
12000 kg with 4 × 2270 kg drop tanks |
| PERFORMANCES | |||
| Maximum Speed | Mach 2.25
(2414 km/h) at altitude |
Supercruise | Mach 1.82 (1963 km/h)
at altitude |
| Range | 2963 km with 2 external fuel tanks |
Ferry Range | 3220 km |
| Combat Radius | 851 km clean with 185 km in supercruise, 1093 km clean subsonic |
Service ceiling | 20000 m |
| Sources | |||
| Wikipédia | - |
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Drawings |
