The first 2 are airplanes of a different generation airplane from J-20.
Now some info from wiki:
General characteristics J-20
Crew: one (pilot)
Length: 21.26 m (69 ft 9 in)
Wingspan: 12.88 m (42 ft 3 in)
Height: 4.45 m (14 ft 7 in)
Wing area: 59 m2 (630 sq ft)
Empty weight: 17,000 kg (37,479 lb)
Max takeoff weight: 36,287 kg (80,000 lb) upper estimate[2]
Powerplant: 2 × WS-10G (prototype); WS-15 when J-20 is serving afterburning turbofans dry, 180 kN (40,000 lbf) with afterburner
Maximum speed: Mach 2.0 or less (DSI limit)[88]
Range: 5,500 km (3,418 mi; 2,970 nmi)
Combat range: 2,000 km (1,243 mi; 1,080 nmi)
Service ceiling: 20,000 m (65,617 ft)
General characteristics - Dessault Rafale
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),[119] 10,196 kg (M) ()
Loaded weight: 14,016 kg (30,900 lb)
Max. takeoff weight: 24,500 kg (C/D), 22,200 kg (M) (54,000 lb)
Powerplant: 2 × Snecma M88-2 turbofans
Dry thrust: 50.04 kN (11,250 lbf) each
Thrust with afterburner: 75.62 kN (17,000 lbf) each
Fuel capacity: 4,700 kg (10,000 lb) internal
Performance
Maximum speed:
High altitude: Mach 1.8+ (2,130+ km/h, 1,050+ knots)
Low altitude: Mach 1.1+ (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 (60,000+ ft/min)
Wing loading: 306 kg/m² (62.8 lb/ft²)
Thrust/weight: 1.10 (100% fuel, 2 EM A2A missile, 2 IR A2A missile)
General characteristics - Eurofighter Typhoon
Crew: 1 (operational aircraft) or 2 (training aircraft)
Length: 15.96 m (52.4 ft)
Wingspan: 10.95 m (35.9 ft)
Height: 5.28 m (17.3 ft)
Wing area: 51.2 m²[231] (551 sq ft)
Empty weight: 11,150 kg (24,600 lb)
Loaded weight: 16,000 kg[231][232] (35,000 lb)
Max. takeoff weight: 23,500 kg (52,000 lb)
Powerplant: 2 × Eurojet EJ200 afterburning turbofan
Dry thrust: 60 kN (13,000 lbf) each
Thrust with afterburner: 89 kN (20,000 lbf) each
Fuel capacity: 4,500 kg (9,900 lb) internal[231]
Performance
Maximum speed:
At altitude: Mach 2 (2,495 km/h/1,550 mph)[233][234][235]
At sea level: Mach 1.2[230] (1,470 km/h/910 mph)[236]
Supercruise: Mach 1.1–1.5[237]
Range: 2,900 km (1,800 mi)
Combat radius:
Ground attack, lo-lo-lo: 601 km (325 nmi)
Ground attack, hi-lo-hi: 1,389 km (750 nmi)
Air defence with 3-hr combat air patrol: 185 km (100 nmi)
Air defence with 10-min. loiter: 1,389 km (750 nmi) [231][238]
Ferry range: 3,790 km (2,350 mi)
Service ceiling: 16,765 m[239] (55,003 ft)
Absolute ceiling: 19,812 m[239] (65,000 ft)
Rate of climb: >315 m/s[240][241] (62,000 ft/min[242])
Wing loading: 312 kg/m²[231] (64.0 lb/ft²
262 kg/m2 with 50% fuel)
Thrust/weight: 1.15
g-limits: +9/−3 g[243]
go on helping yourself elevated to indian military generals
What's this fascination with Chinese Junk series? We don't even know what this latest junk is capable of. Having those big asss canards on a stealth fighter is dumb to say the last.
Chinese Junk-10 plane is famous for being a maintenance nightmare
China Gives J-10s Away and hiding crashes
China tries to hide J-10 fighter crashes . Lets see what this latest junk will become famous for.
As for American Maal, once this MMS fag goes, the govt-govt direct sale nonsense will automatically ground to a Halt. Already plenty of Hangar queens waiting if India decides to do something contrary to GOTUS wishes.
the source quoted above as not in anyway higher than indian slanders. so you guys really serve your masters well!
which of the phase are you in now looking for an effective sealant that can cure the headaches in your Leaking Cockpit Aircraft before it is permanently diplayed in your Museum of indigenous indian failures (miif - myth)! Its the start of Losing Confidence Aircraft projects indeed for india airforce - the run away champions of plane crashes! RIP RIP RIP
Perhaps you need LCA Block II - the Learning Curve Aircraft projects to continue as soon as all the prototypes are downgraded to UAVs