KingOfGods
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it's always funny to read bharti logic
so just because Chinese are not using the JF-17 Thunder means it doesnt count as a gap-filler for PAF - despite the fact that the latter will be far more capable than the Fantans and J-7s of which the ''status quo'' is substantially comprised of
so an aircraft has to be inducted in PLAAF for it to be a threat to hindustan, as per these civilian ''analysts'' with keyboards
No...........The logic was.............JF-17 is not in the same league of other modern fighter aircrafts. It can be a gap-filler; but not a first choice for frontline fighter. Thats why no other country (even who produced it) is buying it as a first choice.
so an aircraft has to be inducted in PLAAF for it to be a threat to hindustan, as per these civilian ''analysts'' with keyboards
PLAAF = a threat to hindustan..................
PAF is much-much better force than PLAAF.............better you guys give them some lessons about flying.
i'm still waiting to see the ''tejas'' get inducted in large numbers
Tejas in question again................Obvious REACTION.
But it always amazes me..................how JF17 and TEJAS are so similar???
Specifications (HAL Tejas)
Data from Aero India 2011, lca-tejas.org, DRDO Techfocus
General characteristics
• Crew: 1
• Length: 13.20 m (43 ft 4 in)
• Wingspan: 8.20 m (26 ft 11 in)
• Height: 4.40 m (14 ft 9 in)
• Wing area: 38.4 m² (413 ft²)
• Empty weight: 6,560 kg (14,460 lb)
• Loaded weight: 10,500 kg (23,100 lb)
• Max takeoff weight: 13,300 kg (29,540 lb)
• Powerplant: 1 × General Electric F404-GE-IN20 turbofan
o Dry thrust: 53.9 kN (11,250 lbf)
o Thrust with afterburner: 85 kN (19,000 lbf)
• G-limits: +9/−3.5 g
• Internal fuel capacity: 2458 kg
• External fuel capacity: 2x1200 litre drop tank at inboard, 1x725 litre drop tank under fuselage.
Performance
• Maximum speed: Mach 1.8 (2,376+ km/h at high altitude) at 15,000 m
• Range: 3,000 km (1,840 mi) without refueling
• Service ceiling: 15,250 m (50,000 ft (engine re-igniter safely capable))
• Wing loading: 221.4 kg/m² (45.35 lb/ft²)
• Thrust/weight: 0.91
Specifications (JF-17/FC-1)
Data from Pakistan Aeronautical Complex
General characteristics
• Crew: 1
• Length: 14.0 m (45.9 ft)
• Wingspan: 9.45 m (including 2 wingtip missiles)[114] (31 ft)
• Height: 4.77 m (15 ft 8 in)
• Wing area: 24.4 m² (263 ft²)
• Empty weight: 6,411 kg (14,134 lb)
• Loaded weight: 9,100 kg (20,062 lb)
• Max takeoff weight: 12,700 kg (28,000 lb)
• Powerplant: 1 × Klimov RD-93 or WS-13 turbofan
o Dry thrust: 49.4 kN / 51.2 kN (11,106 lbf / 11,510 lbf)
o Thrust with afterburner: 84.4 kN / 86.36 kN (18,973 lbf / 19,391 lbf)
• G-limit: +8.5 g
• Internal Fuel Capacity: 2300 kg (5,130 lb)
Performance
• Maximum speed: Mach 1.8 (1,191 knots, 2,205 km/h)
• Combat radius: 1,352 km (840 mi)
• Ferry range: 3,480 km (1,880 NM = 2,160 mi)
• Service ceiling: 16,920 m (55,500 ft)
• Thrust/weight: 0.95