根本不是IDF對手,堪稱是人間第一大笑機
J-10其實比歐洲雙風日本F-2都大
颱風
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[430] (551 sq ft)
Empty weight: 11,000 kg[431][N 6] (24,000 lb)
Loaded weight: 16,000 kg[432][N 7] (35,270 lb)
Max. takeoff weight: 23,500 kg[430] (51,800 lb)
Fuel capacity: 5,000 kg (11,020 lb) internal[433][434]
Powerplant: 2 × Eurojet EJ200 afterburning turbofan
Dry thrust: 60 kN (13,500 lbf) each
Thrust with afterburner: >90 kN[431][435] (20,230 lbf) each
Performance
Maximum speed:
At altitude: Mach 2 class[436] (2,495 km/h or 1,550 mph at 10,975m altitude)[437][438]
At sea level: Mach 1.25[429] (1,530 km/h or 950 mph)[439]
Supercruise: Mach 1.5[175]
Range: 2,900 km (1,800 mi)
Combat radius:
(with 3 × external 1,000 l tanks)
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) [430][440]
Ferry range: >3,790 km (2,350 mi; with 3 × drop tanks)
Service ceiling: 19,812 m (65,000 ft[441][442])
Rate of climb: >318 m/s[443][N 8][444] (62,600 ft/min)
Wing loading: 312 kg/m²[430] (63.9 lb/ft²)
Thrust/weight: 1.15 (interceptor configuration)[430][445]
g-load limits: +9 g to −3 g[446]
Brakes-off to Take-off acceleration: <8 s
Brakes-off to supersonic acceleration: <30 s
Brakes-off to Mach 1.6 at 11,000 m (36,000 ft): <150 s[447][N 9]
陣風
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:
10,300 kilograms (22,700 lb) (B)[70][275]
9,850 kilograms (21,720 lb) (C)[70][275]
10,600 kilograms (23,400 lb) (M)[70][275] ()
Loaded weight: 15,000 kilograms (33,000 lb) ()
Max. takeoff weight: 24,500 kilograms (54,000 lb) (B/C/D) ()
Fuel capacity: 4,700 kg (10,400 lb) internal for single-seater (C); 4,400 kg for two-seater (B)
Powerplant: 2 × Snecma M88-2 turbofans
Dry thrust: 50.04 kN (11,250 lbf) each
Thrust with afterburner: 75 kN (16,860 lbf[279]) each
Performance
Maximum speed:
High altitude: Mach 1.8 (1,912 km/h, 1,032 knots)
Low altitude: Mach 1.1 (1,390 km/h, 750 knots)
Range: >3,700 km (>2,000 nmi) with 3 drop tanks
Combat radius: >1,852 km (>1,000 nmi) on penetration mission with two CFTs (2,300 L), three tanks (5,700 L), two SCALP-EG and two MICA AAMs.
Service ceiling: 15,235 m (50,000 ft)
Rate of climb: >304.8 m/s (>60,000 ft/min)
Wing loading: 328 kg/m2 (67.1 lb/ft2)
Thrust/weight: 0.988 (100% fuel, 2 EM A2A missile, 2 IR A2A missile) version B
Maximum g-load: +9/−3.6g (+11g in emergencies)[61][280][281]
