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| Manufacturer | Boeing Defense Lockheed Martin |
| Category | Fighter Jets Fighter Jets |
| Name | F/A-18E/F Super Hornet F-35 Lightning II |
| Manufacturer | Boeing Defense, Space & Security Lockheed Martin |
| Country of Origin | United States United States |
| Type / Role | Carrier-based Multirole Fighter Multirole Stealth Fighter |
| Generation | 4.5th 5th |
| Status | In active service In Service |
| First Flight | November 29, 1995 December 15, 2006 |
| Introduction / In Service Since | 1999 2015 |
| Number Built | Over 600 units 1,200+ (as of 2025) |
| Operators | U.S. Navy, Royal Australian Air Force USA, UK, Japan, Israel, Italy, Australia, and others |
| Length | 60.3 ft (18.5 m) 51.2 ft (15.6 m) |
| Wingspan | 44.9 ft (13.6 m) 35 ft (10.7 m) |
| Height | 16 ft (4.9 m) 14.4 ft (4.38 m) |
| Wing Area | 500 sq ft (46.5 m²) 460 sq ft (42.7 m²) |
| Empty Weight | 32,081 lb (14,552 kg) 29,300 lb (13,300 kg) |
| Maximum Takeoff Weight (MTOW) | 66,000 lb (29,937 kg) 70,000 lb (31,800 kg) |
| Internal Weapons Bay | None 2 (up to 5,700 lb payload) |
| External Hardpoints | 11 6–10 (up to 18,000 lb total) |
| Maximum Speed | Mach 1.8 Mach 1.6 |
| Range | 1,275 nm (2,346 km) 1,380 mi (2,220 km) |
| Combat Radius | 390 nm (722 km) ~670 mi (1,080 km) |
| Service Ceiling | 50,000 ft (15,240 m) 50,000 ft (15,240 m) |
| Rate of Climb | 44,882 ft/min 45,000 ft/min |
| Thrust-to-Weight Ratio | 0.93 0.87 |
| G Limits | +7.5 / -3.0 +9 |
| Engine Type | Afterburning Turbofan Pratt & Whitney F135-PW-100 |
| No. of Engines | 2 1 |
| Thrust (each) | 22,000 lbf 43,000 lbf |
| Thrust Vectoring | No Yes (on F-35B variant) |
| Fuel Capacity | 14,400 lb (internal) ~18,500 lb internal |
| Gun | 1× M61A2 20mm Vulcan GAU-22/A 25mm cannon (F-35A) |
| Missiles (Air-to-Air) | AIM-9X, AIM-120 AMRAAM AIM-120 AMRAAM, AIM-9X |
| Missiles (Air-to-Ground) | AGM-84 Harpoon, AGM-88 HARM AGM-154 JSOW, AGM-158 JASSM |
| Bombs | JDAM, Paveway, Mk 83/84 JDAM, Paveway II/III, SDB I/II |
| Hardpoints | 11 6 external + 2 internal |
| Payload Capacity | 9,920 kg (21,900 lb) ~18,000 lb |
| Radar | AN/APG-79 AESA AN/APG-81 AESA |
| Radar Range | 150+ km ~150+ km |
| Electronic Warfare (EW) System | AN/ALQ-214 IDECM AN/ASQ-239 suite |
| Targeting System | ATFLIR pod EOTS (Electro-Optical Targeting System) |
| Helmet Display | JHMCS HMDS Gen III |
| Navigation | GPS/INS GPS/INS with terrain-following |
| Autopilot / AI Assistance | Advanced Flight Control System Advanced flight management |
| Communication | Secure data link, Link 16 MADL & Link 16 secure data links |
| Radar Cross Section (RCS) | Reduced (~1 m² class) ~0.001 m² |
| Stealth Features | Radar-absorbent materials, shaping RAM coating, internal weapons bay, edge alignment |
| Infrared Signature Reduction | Moderate Yes |
| Sensor Fusion | Partial Full 360° data integration |
| Networking Capabilities | NIFC-CA compatible Distributed data-sharing with allied units |
| Special Export Versions | Australia (F/A-18F) F-35I (Israel), F-35A (Japan), etc. |
| Major Conflicts / Deployments | Iraq, Afghanistan, Syria, Libya Middle East operations (Iraq, Syria) |
| Notable Operators | U.S. Navy, Australia USAF, USN, USMC, RAF, IDF |
| Combat Proven? | Yes Yes |
| Mission Types | Air superiority, strike, SEAD, maritime patrol Air superiority, strike, SEAD, ISR |
| Unit Cost | ~$70–80 million (Block III) $80–100 million (variant-dependent) |
| Development Cost | ~$5 billion ~$400 billion (program total) |
| Program Name | F/A-18E/F Super Hornet Program Joint Strike Fighter (JSF) |
| Funding Countries | United States, Australia USA, UK, Italy, Netherlands, Canada, Australia, etc. |
| Upgrades Planned | Block III digital cockpit, network enhancements Block 4, Tech Refresh 3 |
| Future Replacement | F/A-XX (Next Generation Air Dominance) NGAD (2035+) |
| Export Restrictions | U.S. ITAR-controlled U.S. FMS approval required |
| Notable Achievements | Over two decades of carrier dominance Widest global fighter program in history |
| Competitors | Rafale M, F-35C, MiG-29K Su-57, J-20, Tempest, KF-21 |
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