| Max Level Speed |
at altitude: 1,355 mph (2,180 km/h) at 30,000 ft (9,150 m), Mach 2 [afterburner]
1,070 mph (1,725 km/h) at 30,000 ft (9,150 m), Mach 1.6 [supercruise]
at sea level: 920 mph (1,480 km/h), Mach 1.2
|
| Initial Climb Rate |
unknown |
| Service Ceiling |
50,000 ft (15,240 m) |
| Range |
typical: 2,000 nm (3,700 km)
ferry: unknown
|
| Endurance |
unknown |
| G-Limits |
+9.0 / -3.0 |
| YF-22 |
Prototype evaluated under the Advanced Tactical Fighter competition; 2 built |
| F-22A |
Production model with a slightly shorter fuselage, reduced wing sweep, and the cockpit shifted forward to improve visibilty; approximately 180 to be built |
| F/A-22A |
Designation given to the F-22A in 2002 to highlight the plane's air-to-ground combat capabilities, but dropped upon service entry in 2005 when the design was again called the F-22A |
| F-22B |
Proposed two-seat combat-capable trainer; cancelled |
| F-22E |
Lockheed proposal for an upgraded version based on the F-22A but with improved ground attack capability |
| F-22N |
Proposed navalized variant with variable-sweep wings for operation from US Navy aircraft carriers; not developed |
| F/A-22X |
Proposed advanced variant that would add a synthetic aperture radar, moving target indicator, and additional ground attack capability |
| FB-22 |
Lockheed concept for a long-range high-altitude bomber based on the F-22; design would eliminate all tail surfaces, incorporate a new delta wing with increased fuel capacity, and employ a longer fuselage with room for stretched weapons bays carrying two AIM-120 missiles and up to 24 small diameter bombs; the Air Force has indicated that it will not order the design |