Lockheed Martin F-22 Raptor
Flat Wing Aspect Ratio
2.36
Entry Into service
2005-12-15
Maximum Take-Off Weight
38 t (paragliders: kg)
Total Fuel Capacity
2271.247
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Aircraft Weight Variants
| Aircraft |
Maximum Take-Off Weight (t (paragliders: kg)) |
Total Fuel Capacity |
Maximum Range (km) |
|
Lockheed Martin F-22 Raptor |
38 |
2271.247 |
2963.2 |
Similar airplanes
All data (27 fields)
- Name
- Lockheed Martin F-22 Raptor
- Manufacturer
- Lockheed Martin
- Description
- The Lockheed Martin–Boeing F-22 Raptor is an American twin-engine, jet-powered, all-weather, supersonic stealth fighter aircraft.
- ICAO Code
- F22
- First Flight
- 1997-09-07
- Entry Into service
- 2005-12-15
- Production End
- 2011-01-01
- Designer
- Lockheed Martin
- Type
- Air superiority fighter
- Length (m)
- 18.92
- Height (m)
- 5.08
- Cockpit Crew
- 1
- Max Ceiling (m)
- 19812
- Armament
- Guns: 1× 20 mm M61A2 Vulcan rotary cannon, 480 rounds; Internal weapons bays:; 8× internal weapon stations for a combination of:; Air-to-air mission loadout:; 6× AIM-120C/D AMRAAM or ; 4× AIM-120A/B; 2× AIM-9M/X Sidewinder; Air-to-ground mission loadout:; 2× 1000 lb JDAM and 2× AIM-120 or; 8× 250 lb GBU-39 SDB and 2× AIM-120 or; 4× 250 lb GBU-39 and 4× AIM-120; 2× AIM-9; Hardpoint (external):; 4×…
- Max Mach (Mach)
- 2.25
- National Origin
- United States of America
- Number Built
- 195
- Powerplant Description
- 2 × Pratt & Whitney F119-PW-100 augmented turbofans, 116 kN thrust each
- Primary Users
- United States Air Force
- Status
- In service
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Lockheed_Martin_F-22_Raptor
- Flat Wing Span (m)
- 13.56
- Flat Wing Area (m²)
- 78.04
- Flat Wing Aspect Ratio
- 2.36
- Wake Category
- M
- Aircraft Engine
- Pratt & Whitney F119
- Number of Engines
- 2