



| Airplane: Lockheed F104 Starfighter Type: Multi-purpose fighter HISTORY: | |
| First Flight | (XF-104) 7 February 1954 |
| Service Entry | January 1958 |
| Retirement | (F-104S) 27 October 2004 |
| CREW: | 1 pilot |
| ESTIMATED COST: | unknown |
| AIRFOIL SECTIONS: | |
| Wing Root | Biconvex 3.36% |
| Wing Tip | Biconvex 3.36% |
| DIMENSIONS: | |
| Length | 54.75 ft (16.69 m) |
| Wingspan | 21.92 ft (6.68 m) |
| Height | 13.50 ft (4.11 m) |
| Wing Area | 196.1 ft2 (18.22 m2) |
| Canard Area | not applicable |
| WEIGHTS: | |
| Empty | 14,082 lb (6,387 kg) |
| Typical Load | unknown |
| Max Takeoff | 28,779 lb (13,054 kg) |
| Fuel Capacity | internal: 5,822 lb (2,641 kg) external: 5,538 lb (2,512 kg) |
| Max Payload | 4,310 lb (1,995 kg) |
| PROPULSION: | |
| Powerplant | one General Electric J79-19 turbojet |
| Thrust | 10,000 lb (44.5 kN) 15,800 lb (70.28 kN) with afterburner |
| PERFORMANCE: | |
| Max Level Speed | at altitude: 1,450 mph (2,335 km/h) at 36,000 ft (10,975 m), Mach 2.2 at sea level: Mach 1.2 |
| Initial Climb Rate | 50,000 ft (15,239 m) / min |
| Service Ceiling | 58,000 ft (17,680 m) 90,000 ft (27,430 m) zoom ceiling |
| Range | typical: 260 nm (480 km) with max payload ferry: 1,576 nm (2,920 km) |
| g-Limits | unknown |
| ARMAMENT: | |
| Gun | one 20-mm M61A1 Vulcan cannon (750 rds) |
| Stations | 7 external hardpoints and 2 wingtip rails |
| Air-to-Air Missile | AIM-9 Sidewinder, AIM-7 Sparrow, Apside |
| Air-to-Surface Missile | AGM-65 Maverick, Kormoran, Penguin |
| Bomb | nuclear bombs, Mk 82/83 GP, cluster bombs |
| Other | rocket pods, ECM pods |
| KNOWN VARIANTS: | |
| XF-104 | Prototype |
| YF-104 | Pre-production aircraft used to test different engines; 17 built |
| F-104A | Production model for the USAF with blown flaps to reduce landing speeds; 153 built |
| NF-104A | F-104A airframes used for astronaut training; 3 converted |
| QF-104A | YF-104 and F-104A aircraft used as radio-controlled target drones |
| F-104B | Two-seat trainer based on the F-104A but with new fuel system and armament layout; 26 built |
| F-104C | Upgraded one-seat tactical fighter bomber used by the USAF with a new engine and armed with Sidewinder missiles, bombs, or rocket pods; 77 built |
| F-104D | Two-seat trainer based on the F-104C model; 21 built |
| CF-104D | Canadian two-seat trainer built under license; 38 built |
| F-104DJ | Two-seat trainer for Japan; 20 built |
| F-104F | Improved attack fighter based on the F-104D model and sold to Germany; 30 built |
| F-104G | German multi-role fighter with ground attack capability, aerodynamic refinements, stronger airframe, more advanced avionics, and a new engine; 1,127 built for European countries |
| TF-104G | German two-seat trainer; 220 built |
| RF-104G | German reconnaissance model with a camera pod in place of the Vulcan cannon; 189 built |
| RTF-104G | Two-seat trainer that can be equipped for reconnaissance duties |
| CF-104 | Canadian multi-role fighter based on the F-104G and built under license; 200 built |
| F-104J | Japanese multi-role fighter based on the F-104G and built under license; 210 built |
| F-104N | F-104G aircraft built for NASA as supersonic chase planes |
| F-104S | Multi-role fighter based on the F-104G and built by Aeritalia for Italy and Turkey, last operational version; 245 built |
| F-104S ASA | Italian F-104S models upgraded by Aeritalia/Alenia under the Aggiornamento Sistemi d'Arma program with new radar, avionics, and weapon systems; 150 converted |
| F-104S ASA M | Final modernization program to keep the Italian F-104S ASA fleet in service into the 21st century by replacing outdated power systems and navigation avionics to improve maintainability; approximately 100 converted |
| KNOWN COMBAT RECORD: | Vietnam War (USAF, 1965-1968) Bangladesh War (Pakistan, 1971) |
| KNOWN OPERATORS: | US Air Force Belgium Canada Denmark German Air Force German Navy Greece Italy Japan Netherlands Norway Pakistan Spain Taiwan Turkey |
| 3-VIEW SCHEMATIC:
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