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| Manufacturer | Airbus Lockheed Martin |
| Category | Fighter Jets Fighter Jets |
| Name | Eurofighter Typhoon F-35 Lightning II |
| Manufacturer | Airbus, BAE Systems, Leonardo Lockheed Martin |
| Country of Origin | UK / Germany / Italy / Spain United States |
| Type / Role | Multirole Fighter Multirole Stealth Fighter |
| Generation | 4.5th 5th |
| Status | Active Service In Service |
| First Flight | March 27, 1994 December 15, 2006 |
| Introduction / In Service Since | 2003 2015 |
| Number Built | 600+ 1,200+ (as of 2025) |
| Operators | UK, Germany, Italy, Spain, Saudi Arabia, Qatar, Austria, Kuwait USA, UK, Japan, Israel, Italy, Australia, and others |
| Length | 15.96 m (52.4 ft) 51.2 ft (15.6 m) |
| Wingspan | 10.95 m (35.9 ft) 35 ft (10.7 m) |
| Height | 5.28 m (17.3 ft) 14.4 ft (4.38 m) |
| Wing Area | 51.2 m² 460 sq ft (42.7 m²) |
| Empty Weight | 11,000 kg 29,300 lb (13,300 kg) |
| Maximum Takeoff Weight (MTOW) | 23,500 kg 70,000 lb (31,800 kg) |
| Internal Weapons Bay | None 2 (up to 5,700 lb payload) |
| External Hardpoints | 13 6–10 (up to 18,000 lb total) |
| Maximum Speed | Mach 2.0 (2,495 km/h) Mach 1.6 |
| Range | 2,900 km 1,380 mi (2,220 km) |
| Combat Radius | 1,390 km ~670 mi (1,080 km) |
| Service Ceiling | 55,000 ft 50,000 ft (15,240 m) |
| Rate of Climb | 62,000 ft/min 45,000 ft/min |
| Thrust-to-Weight Ratio | 1.15 0.87 |
| G Limits | +9g +9 |
| Engine Type | Eurojet EJ200 Turbofan Pratt & Whitney F135-PW-100 |
| No. of Engines | 2 1 |
| Thrust (each) | 20,000 lbf 43,000 lbf |
| Thrust Vectoring | Optional (prototype) Yes (on F-35B variant) |
| Fuel Capacity | ~5,000 kg internal ~18,500 lb internal |
| Gun | 1× 27mm Mauser BK-27 cannon GAU-22/A 25mm cannon (F-35A) |
| Missiles (Air-to-Air) | AIM-120 AMRAAM, Meteor, IRIS-T AIM-120 AMRAAM, AIM-9X |
| Missiles (Air-to-Ground) | Brimstone, Storm Shadow AGM-154 JSOW, AGM-158 JASSM |
| Bombs | Paveway IV, JDAM JDAM, Paveway II/III, SDB I/II |
| Hardpoints | 13 6 external + 2 internal |
| Payload Capacity | 9,000 kg ~18,000 lb |
| Radar | Captor-E AESA AN/APG-81 AESA |
| Radar Range | ~160 km ~150+ km |
| Electronic Warfare (EW) System | DASS suite AN/ASQ-239 suite |
| Targeting System | Litening III pod EOTS (Electro-Optical Targeting System) |
| Helmet Display | Striker II HMDS Gen III |
| Navigation | INS/GPS GPS/INS with terrain-following |
| Autopilot / AI Assistance | Digital flight control Advanced flight management |
| Communication | Secure data link, MIDS MADL & Link 16 secure data links |
| Radar Cross Section (RCS) | ~1–2 m² ~0.001 m² |
| Stealth Features | Reduced radar signature materials RAM coating, internal weapons bay, edge alignment |
| Infrared Signature Reduction | Moderate Yes |
| Sensor Fusion | Advanced data integration Full 360° data integration |
| Networking Capabilities | NATO Link-16, future FCAS integration Distributed data-sharing with allied units |
| Special Export Versions | Kuwait, Qatar (enhanced avionics) F-35I (Israel), F-35A (Japan), etc. |
| Major Conflicts / Deployments | Libya (2011), Baltic Air Policing Middle East operations (Iraq, Syria) |
| Notable Operators | RAF, Luftwaffe, Italian Air Force USAF, USN, USMC, RAF, IDF |
| Combat Proven? | Yes Yes |
| Mission Types | Air superiority, strike, reconnaissance Air superiority, strike, SEAD, ISR |
| Unit Cost | ~$95 million $80–100 million (variant-dependent) |
| Development Cost | ~$45 billion total ~$400 billion (program total) |
| Program Name | Eurofighter Program Joint Strike Fighter (JSF) |
| Funding Countries | UK, Germany, Italy, Spain USA, UK, Italy, Netherlands, Canada, Australia, etc. |
| Upgrades Planned | Radar and weapons modernization Block 4, Tech Refresh 3 |
| Future Replacement | FCAS (Future Combat Air System) NGAD (2035+) |
| Export Restrictions | Limited by EU arms policy U.S. FMS approval required |
| Notable Achievements | Key NATO air defense asset Widest global fighter program in history |
| Competitors | F-16V, Rafale, Gripen E Su-57, J-20, Tempest, KF-21 |
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