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| I am posting all the data I could get from Wikipedia. 1) JAS 39 Gripen
General characteristics
* Crew: 1 (2 for JAS 39B/D)
* Length: 14.1 m (46 ft 3 in)
* Wingspan: 8.4 m (27 ft 7 in)
* Height: 4.5 m (14 ft 9 in)
* Wing area: 30.0 m² (323 ft²)
* Empty weight: 5,700 kg (14,600 lb)
* Loaded weight: 8,500 kg (18,700 lb)
* Max takeoff weight: 14,000 kg (31,000 lb)
* Powerplant: 1× Volvo Aero RM12 afterburning turbofan
o Dry thrust: 54 kN (12,100 lbf)
o Thrust with afterburner: 80.5 kN (18,100 lbf)
* Wheel track: 2.4 m (7 ft 10 in)
* Length (two-seater): 14.8 m (48 ft 5 in)
Performance
* Maximum speed:
o At altitude: Mach 2 (2,130 km/h, 1,320 mph)
* Combat radius: 800 km (500 mi, 432 nmi)
* Ferry range: 3,200 km (2,000 mi) with drop tanks
* Service ceiling: 15,240 m (50,000 ft)
* Wing loading: 336 kg/m² (68.8 lb/ft²)
* Thrust/weight: 0.97 2) F/A-18E/F Super Hornet
Specifications (F/A-18E/F)
General characteristics
* Crew: F/A-18E: 1, F/A-18F: 2
* Length: 60 ft 1¼ in (18.31 m)
* Wingspan: 44 ft 8½ in (13.62 m)
* Height: 16 ft (4.88 m)
* Wing area: 500 ft² (46.45 m²)
* Empty weight: 30,600 lb (13,900 kg)
* Loaded weight: 47,000 lb (21,320 kg) (in fighter configuration)
* Max takeoff weight: 66,000 lb (29,900 kg)
* Powerplant: 2× General Electric F414-GE-400 turbofans
o Dry thrust: 14,000 lbf (62.3 kN) each
o Thrust with afterburner: 22,000 lbf (97.9 kN) each
* Internal fuel capacity: F/A-18E: 14,400 lb (6,530 kg), F/A-18F: 13,550 lb (6,145 kg)
* External fuel capacity: 5 × 480 gal tanks, totaling 16,380 lb (7,430 kg)
Performance
* Maximum speed: Mach 1.8[12] (1,190 mph, 1,900 km/h) at 40,000 ft (12,190 m)
* Range: 1,275 nmi (2,346 km) clean plus two AIM-9s[12]
* Combat radius: 390 nmi (449 mi, 722 km) for interdiction mission[82]
* Ferry range: 1,800 nmi (2,070 mi, 3,330 km)
* Service ceiling: 50,000+ ft (15,000+ m)
* Wing loading: 92.8 lb/ft² (453 kg/m²)
* Thrust/weight: 0.93 3) Eurofighter Typhoon
General characteristics
* Crew: 1 (operational aircraft) or 2 (training aircraft)
* Length: 15.96 m (52 ft 5 in)
* Wingspan: 10.95 m (35 ft 11 in)
* Height: 5.28 m (17 ft 4 in)
* Wing area: 50 m² (538 ft²)
* Empty weight: 11,000 kg (24,250 lb)
* Loaded weight: 15,550 kg (34,280 lb)
* Max takeoff weight: 23,500 kg (51,800 lb)
* Powerplant: 2× Eurojet EJ200 afterburning turbofan
o Dry thrust: 60 kN (13,500 lbf) each
o Thrust with afterburner: 90 kN (20,000 lbf) each
Performance
* Maximum speed:
o At altitude: Mach 2+ (2,495 km/h, 1550 mph)[168][169]
o At sea level: Mach 1.2
o Supercruise: Mach 1.1[167]-1.5[170]
* Range: 2,900 km (1,840 mi)
* Combat radius:
o Ground attack, lo-lo-lo : 601 km (373nm)
o Ground attack, hi-lo-hi : 1389 km (863 nm)
o Air defence with 3hr CAP : 185 km (115nm)
o Air defence with 10-min loiter : 1389 km (863 mi) [171] ()
* Ferry range: 3,790 km (2,300 mi)
* Service ceiling: 19,812 m (65,000 ft)
* Rate of climb: >315 m/s[172][173] (62,000 ft/min[174])
* Wing loading: 311 kg/m² (63.7 lb/ft²)
* Thrust/weight: 1.16 4) Lockheed Martin F 16 IN
General characteristics
* Crew: 1
* Length: 49 ft 5 in (14.8 m)
* Wingspan: 32 ft 8 in (9.8 m)
* Height: 16 ft (4.8 m)
* Wing area: 300 ft² (27.87 m²)
* Airfoil: NACA 64A204 root and tip
* Empty weight: 18,900 lb (8,670 kg)
* Loaded weight: 26,500 lb (12,000 kg)
* Max takeoff weight: 42,300 lb (19,200 kg)
* Powerplant: 1× F110-GE-100 afterburning turbofan
o Dry thrust: 17,155 lbf (76.3 kN)
o Thrust with afterburner: 28,600 lbf (128.9 kN)
Performance
* Maximum speed:
o At sea level: Mach 1.2 (915 mph, 1,470 km/h)
o At altitude: Mach 2+ (1,500 mph, 2,414 km/h)
* Combat radius: 340 mi (295 nm, 550 km) on a hi-lo-hi mission with six 1,000 lb (450 kg) bombs
* Ferry range: 2,280 NM (2,620 mi, 4,220 km) with drop tanks
* Service ceiling: 60,000+ ft (18,000+ m)
* Rate of climb: 50,000 ft/min (254 m/s)
* Wing loading: approx 40 lb/ft²[142] (430 kg/m²)
* Thrust/weight: 1.095 5) Mikoyan MIG 35
General characteristics
* Crew: one or two
* Length: 19 m (62 ft 4 in)
* Wingspan: 15 m (49 ft 3 in)
* Height: 6 m (19 ft 8 in)
* Empty weight: 11,000 kg (24,250 lb)
* Loaded weight: 17,500 kg (38,600 lb)
* Max takeoff weight: 29,700 kg (65,500 lb)
* Powerplant: 2× Klimov RD-33MK afterburning turbofans
o Dry thrust: 5,400 kgf, 53.0 kN (11,900 lbf) each
o Thrust with afterburner: 9,000 kgf, 88.3 kN (19,800 lbf) each
Performance
* Maximum speed: Mach 2.25 (2,400 km/h, 1,491 mph) at altitude
* Range: 2,000 km (1,240 mi)
* Ferry range: 3,100 km (1,930 mi) with 3 external fuel tanks
* Service ceiling: 17,500 m (57,400 ft)
* Rate of climb: 330 m/s (65,000 ft/min)
* Thrust/weight: 1.14 6) Dassault Rafale
General characteristics
* Crew: 1–2
* Length: 15.27 m (50.1 ft)
* Wingspan: 10.80 m (35.4 ft)
* Height: 5.34 m (17.5 ft)
* Wing area: 45.7 m² (492 ft²)
* Empty weight: 9,500 kg (C), 9,770 kg (B),[57] 10,196 kg (M) ()
* Max takeoff weight: 24,500 kg (C/D), 22,200 kg (M)[58] (54,000 lb)
* Powerplant: 2× Snecma M88-2 turbofans
o Dry thrust: 50.04 kN (11,250 lbf) each
o Thrust with afterburner: 75.62 kN with M88-Eco >90 kN after 2010 (17,000 lbf) each
Performance
* Maximum speed:
o High altitude: Mach 2 (1,290 knots)[57]
o Low altitude: 1,390 km/h, 750 knots
* Range: 3,700+ km (2,000+ nmi)
* Combat radius: 1,852+ km (1,000+ nmi) on penetration mission
* Service ceiling: 16,800 m (55,000 ft)
* Rate of climb: 304.8+ m/s (1,000+ ft/s)
* Wing loading: 326 kg/m² (83 1/3 lb/ft²)
* Thrust/weight: 1.13 |