| Manufacturer |
Lockheed Martin |
|---|
| Role |
Fifth generation, multi role fighter |
|---|
| Crew |
Pilot |
|---|
| Engines |
Pratt & Whitney F135-PW-100 |
|---|
| Airframe |
Length: 15.7 m, height: 4.4 m |
|---|
| Wingspan |
10.7 m |
|---|
| Wing Area |
42.7m2 |
|---|
| Weight |
13,290 kg (empty), 29,900 kg (max) |
|---|
| Range |
2,200 km |
|---|
| Combat radius (internal fuel) |
1093 km |
|---|
| Internal Fuel Capacity |
8278 kg |
|---|
| Ceiling |
50,000 feet |
|---|
| Max Speed |
1,960 km/h (Mach 1.6) |
|---|
| Thrust |
40,000 lb Maximum power (with afterburner), 25,000 lb Military Power (without afterburner) |
|---|
| Max g-rating |
9.0 |
|---|
| Capability |
- Low Observation Stealth
- Advanced sensors
- Networking and Data Fusion Capabilities
- Helmet Mounted Sight
|
|---|
| Weapons |
- AIM-120C Air-to-Air Missile
- AIM-9X "Sidewinder" Short Range Air-toAir Missile
- GBU-31 Joint Direct Attack Munitions (JDAM) Guided Bombs
- Laser-Guided Bombs
- Internal 25 mm GAU-22/A Cannon
|
|---|
| Weapon Payload |
8160 kg |
|---|
