F-22A Raptor at 2008 Andrews AFB airshow
The F-22 is a jet fighter of the 5th generation capacity stealth 5th generation. It has two engines turbofan with afterburning Pratt & Whitney F119-PW-100 capable of vectored thrust . The maximum thrust is a classified information , even if most of the sources gives the value of 156 k N for propulsor. It is estimated a maximum speed of around Mach 1.82 mode Supercruise (ie without the use of afterburners ).
| Description | |
|---|---|
| Type | air superiority fighter of V generation stealth |
| Crew | 1 pilot |
| Builder |  Lockheed Martin Boeing IDS |
| Date first flight | 27 September 1990 (YF-22) |
| Date of entry into service | December 15, 2005 (F-22A) |
| Primary user | USAF |
| Specimens | 187 |
| Unit cost | 138 million U.S. $ |
| Developed by | YF-22 Lightening II |
| Other variants | X-44 MANTA |
| Dimensions and weights | |
 | |
| Length | 18.90 m (62 ft 1 in ) |
| Wingspan | 13.56 m (44 ft 6 in) |
| Wing area | 78.04 m² (840 ft ²) |
| Wing loading | 322 kg / m² (66 lb / ft ²) |
| Empty weight | 19 700 kg (43,430 lb ) (The truth is, a given weight assigned, and varies depending on the source, between 14 and 19 tons) |
| Weight load | 29 300 kg (64,460 lb) [1] |
| Maximum takeoff weight | 38 000 kg (83,500 lb) |
| Propulsion | |
| Engine | 2 turbofan Pratt & Whitney F119-PW-100 with afterburner |
| Push | from 104 to 156 kN each |
| Performance | |
| Max | 2.25 But (2410 km / h at high altitude) [2] |
| Autonomy | 2960 km |
| Range | 759 km |
| Tangency | 19 812 m |
| Armament | |
| Cannons | 1 M61A2 Vulcan 20mm |
| Bombs | free fall: 8 GBU-39 GPS guidance: 2 JDAM 2 WCMD |
| Missiles | air-to-air: 2 AIM-9 Sidewinder 6 AIM-120 AMRAAM |
| Pylons | 4 underwing 2 holds internal |
| More | version information: F-22A 'Raptor' |
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