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Specifications (F-5E Tiger II) Data from Quest for Performance[20] General characteristics * Crew: 1 * Length: 47 ft 4¾ in (14.45 m) * Wingspan: 26 ft 8 in (8.13 m) * Height: 13 ft 4½ in (4.08 m) * Wing area: 186 ft² (17.28 m²) * Airfoil: NACA 65A004.8 root, NACA 64A004.8 tip * Empty weight: 9,558 lb (4,349 kg) * Max takeoff weight: 24,664 lb (11,187 kg) * Powerplant: 2× General Electric J85-GE-21B turbojet ** Dry thrust: 3,500 lbf (15.5 kN) each ** Thrust with afterburner: 5,000 lbf (22.2 kN) each * *Zero-lift drag coefficient: 0.0200 * Drag area: 3.4 ft² (0.32 m²) * Aspect ratio: 3.86 * Internal fuel: 677 US gal (2,563 L) * External fuel: 275 US gal (1,040 L) per tank in up to 3 tanks Performance * Maximum speed: 917 kn (1,060 mph, 1,700 km/h, mach 1.6) * Range: 760 nmi (870 mi, 1,405 km) * Ferry range: 2,010 nmi (2,310 mi, 3,700 km[21]) * Service ceiling: 51,800 ft (15,800 m) * Rate of climb: 34,400 ft/min (175 m/s) * Lift-to-drag ratio: 10.0 from the T-38 Wikipedia page (varient of the F-5)Performance* Maximum speed: Mach 1.3 (858 mph, 1,381 km/h) * Range: 1,140 mi (1,835 km) * Service ceiling: 50,000 ft (15,240 m) * Rate of climb: 33,600 ft/min (170.7 m/s) * Wing loading: 70 lb/ft² (340 kg/m²) * Thrust/weight:0.65 Specifications (F-5E Tiger II) Data from Quest for Performance[20] General characteristics * Crew: 1 * Length: 47 ft 4¾ in (14.45 m) * Wingspan: 26 ft 8 in (8.13 m) * Height: 13 ft 4½ in (4.08 m) * Wing area: 186 ft² (17.28 m²) * Airfoil: NACA 65A004.8 root, NACA 64A004.8 tip * Empty weight: 9,558 lb (4,349 kg) * Max takeoff weight: 24,664 lb (11,187 kg) * Powerplant: 2× General Electric J85-GE-21B turbojet ** Dry thrust: 3,500 lbf (15.5 kN) each ** Thrust with afterburner: 5,000 lbf (22.2 kN) each * *Zero-lift drag coefficient: 0.0200 * Drag area: 3.4 ft² (0.32 m²) * Aspect ratio: 3.86 * Internal fuel: 677 US gal (2,563 L) * External fuel: 275 US gal (1,040 L) per tank in up to 3 tanks Performance * Maximum speed: 917 kn (1,060 mph, 1,700 km/h, mach 1.6) * Range: 760 nmi (870 mi, 1,405 km) * Ferry range: 2,010 nmi (2,310 mi, 3,700 km[21]) * Service ceiling: 51,800 ft (15,800 m) * Rate of climb: 34,400 ft/min (175 m/s) * Lift-to-drag ratio: 10.0 from the T-38 Wikipedia page (varient of the F-5)Performance* Maximum speed: Mach 1.3 (858 mph, 1,381 km/h) * Range: 1,140 mi (1,835 km) * Service ceiling: 50,000 ft (15,240 m) * Rate of climb: 33,600 ft/min (170.7 m/s) * Wing loading: 70 lb/ft² (340 kg/m²) * Thrust/weight:0.65

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