killerx
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FC20 VS MIG29UPG FC20 is being acquired by PAF and IAF is upgrading its mig29 to UPG package which would win the battle if come face to face in WVR & BVR combat.
J-10B
numerous images of a new J-10 variant have surfaced, showing a prototype J-10 modified with increased RAM, MAW, a diverterless supersonic inlet (DSI), an infra-red search and track (IRST) sensor, modified vertical stabiliser, ventral fins, housings fitted under the wings, next generation of integrated electronics, and a modified nose with an AESA radar.It had its first flight in December 2008.
Note these specifications are of J10A and J10B full specifications have to yet confirmed after the full operational delivered to PAF
Specifications (J-10A)
General characteristics
Crew: 1 (basic), 2 (trainer variant)
Length: 16.43 m [29] (53 ft 10 in)
Wingspan: 9.75 m [29] (31 ft 11 in)
Height: 4.78 m (15.7 ft)
Wing area: 39 m² (419.8 ft²)
Empty weight: 9,750 kg (21,495 lb)
Loaded weight: 14,876 kg (32,797 lb)
Useful load: 4,500 kg[43][44] (9,920 lb)
Max takeoff weight: 19,277 kg (42,500 lb)
Powerplant: 1 × Saturn-Lyulka AL-31FN or WS-10A Taihang turbofan
Dry thrust: 79.43 kN / 89.17 kN (17,860 lbf / 20,050 lbf)
Thrust with afterburner: 122.5 kN[11] / 132 kN (27,557 lbf / 29,101 lbf)
Performance
Maximum speed: Mach 2.2 at altitude, Mach 1.2 at sea level
g-limits: +9/-3 g (+88/-29 m/s², +290/-97 ft/s²[7)
Combat radius: 1600 km[46] with in-flight refueling
1100 km without in flight refueling[35] ()
Ferry range: 3200 km
Service ceiling: 20,300 m (66,601 ft )
Wing loading: 335 kg/m² (69 lb/ft²)
Thrust/weight: 0.98 (with AL-31); 1.03 (with WS-10A)
Armament
Guns: 1× 23mm twin-barrel cannon
Hardpoints: 11 in total (6× under-wing, 5× under-fuselage) with a capacity of 6,000 kg (13,228 lb) external fuel and ordnance
Rockets: 90 mm unguided rocket pods
Missiles:
Air-to-air missiles: PL-8, PL-9, PL-11, PL-12
Air-to-surface missiles: PJ-9, YJ-9K
Bombs: laser-guided bombs (LT-2), glide bombs (LS-6) and unguided bombs
Others:
Up to 3 external fuel drop-tanks (1× under-fuselage, 2× under-wing) for extended range and loitering time
Avionics
Unnamed phased array radar
NRIET KLJ-10 multi-mode fire-control radar
Externally-mounted avionics pods:
Type Hongguang-I infra-red search and track pod
BM/KG300G self-protection jamming pod
KZ900 electronic reconnaissance pod
Blue Sky navigation/attack pod
FILAT (Forward-looking Infra-red Laser Attack Targeting) pod
MiG-29UPG
The design is a new modification intended for the MiG-29s used by Indian Air Force. It made its maiden flight on 4 February 2011. The standard includes the new Zhuk-M radar, new avionics, a IFR probe as well as new enhanced RD-33 series 3 turbojet engines. The modernization is part of a $900 million contract to upgrade the 69 fighters fleet.
General characteristics
Crew: 1
Length: 17.37 m (57 ft)
Wingspan: 11.4 m (37 ft 3 in)
Height: 4.73 m (15 ft 6 in)
Wing area: 38 m² (409 ft²)
Empty weight: 11,000 kg (24,250 lb)
Loaded weight: 15,300 kg (33,730 lb)
Max takeoff weight: 20,000 kg (44,100 lb)
Powerplant: 2 × Klimov RD-33 afterburning turbofans, 8,300 kgf (81.4 kN, 18,300 lbf) each
Performance
Maximum speed: Mach 2.25 (2,400 km/h, 1,490 mph) At low altitude: Mach 1.25 (1,500 km/h, 930 mph)
Range: 1,430 km (772 nmi, 888 mi) with maximum internal fuel
Ferry range: 2,100 km (1,300 mi) with 1 drop tank
Service ceiling: 18,013 m (59,100 ft)
Rate of climb: initial 330 m/s average 109 m/s 06000 m[126] (65,000 ft/min)
Wing loading: 442 kg/m² (90.5 lb/ft²)
Thrust/weight: 1.08
Armament
1 x 30 mm GSh-30-1 cannon with 150 rounds
7 Hard points: 6 x pylons under-wing, 1 x under fuselage
Up to 3,500 kg (7,720 lb) of weapons including six air-to-air missiles a mix of semi-active radar homing (SARH) and AA-8 "Aphid", AA-10 "Alamo", AA-11 "Archer", AA-12 "Adder", FAB 500-M62, FAB-1000, TN-100, ECM Pods, S-24, AS-12, AS-14
Avionics
Phazotron N019, N010 radars
J-10B
numerous images of a new J-10 variant have surfaced, showing a prototype J-10 modified with increased RAM, MAW, a diverterless supersonic inlet (DSI), an infra-red search and track (IRST) sensor, modified vertical stabiliser, ventral fins, housings fitted under the wings, next generation of integrated electronics, and a modified nose with an AESA radar.It had its first flight in December 2008.
Note these specifications are of J10A and J10B full specifications have to yet confirmed after the full operational delivered to PAF
Specifications (J-10A)
General characteristics
Crew: 1 (basic), 2 (trainer variant)
Length: 16.43 m [29] (53 ft 10 in)
Wingspan: 9.75 m [29] (31 ft 11 in)
Height: 4.78 m (15.7 ft)
Wing area: 39 m² (419.8 ft²)
Empty weight: 9,750 kg (21,495 lb)
Loaded weight: 14,876 kg (32,797 lb)
Useful load: 4,500 kg[43][44] (9,920 lb)
Max takeoff weight: 19,277 kg (42,500 lb)
Powerplant: 1 × Saturn-Lyulka AL-31FN or WS-10A Taihang turbofan
Dry thrust: 79.43 kN / 89.17 kN (17,860 lbf / 20,050 lbf)
Thrust with afterburner: 122.5 kN[11] / 132 kN (27,557 lbf / 29,101 lbf)
Performance
Maximum speed: Mach 2.2 at altitude, Mach 1.2 at sea level
g-limits: +9/-3 g (+88/-29 m/s², +290/-97 ft/s²[7)
Combat radius: 1600 km[46] with in-flight refueling
1100 km without in flight refueling[35] ()
Ferry range: 3200 km
Service ceiling: 20,300 m (66,601 ft )
Wing loading: 335 kg/m² (69 lb/ft²)
Thrust/weight: 0.98 (with AL-31); 1.03 (with WS-10A)
Armament
Guns: 1× 23mm twin-barrel cannon
Hardpoints: 11 in total (6× under-wing, 5× under-fuselage) with a capacity of 6,000 kg (13,228 lb) external fuel and ordnance
Rockets: 90 mm unguided rocket pods
Missiles:
Air-to-air missiles: PL-8, PL-9, PL-11, PL-12
Air-to-surface missiles: PJ-9, YJ-9K
Bombs: laser-guided bombs (LT-2), glide bombs (LS-6) and unguided bombs
Others:
Up to 3 external fuel drop-tanks (1× under-fuselage, 2× under-wing) for extended range and loitering time
Avionics
Unnamed phased array radar
NRIET KLJ-10 multi-mode fire-control radar
Externally-mounted avionics pods:
Type Hongguang-I infra-red search and track pod
BM/KG300G self-protection jamming pod
KZ900 electronic reconnaissance pod
Blue Sky navigation/attack pod
FILAT (Forward-looking Infra-red Laser Attack Targeting) pod
MiG-29UPG
The design is a new modification intended for the MiG-29s used by Indian Air Force. It made its maiden flight on 4 February 2011. The standard includes the new Zhuk-M radar, new avionics, a IFR probe as well as new enhanced RD-33 series 3 turbojet engines. The modernization is part of a $900 million contract to upgrade the 69 fighters fleet.
General characteristics
Crew: 1
Length: 17.37 m (57 ft)
Wingspan: 11.4 m (37 ft 3 in)
Height: 4.73 m (15 ft 6 in)
Wing area: 38 m² (409 ft²)
Empty weight: 11,000 kg (24,250 lb)
Loaded weight: 15,300 kg (33,730 lb)
Max takeoff weight: 20,000 kg (44,100 lb)
Powerplant: 2 × Klimov RD-33 afterburning turbofans, 8,300 kgf (81.4 kN, 18,300 lbf) each
Performance
Maximum speed: Mach 2.25 (2,400 km/h, 1,490 mph) At low altitude: Mach 1.25 (1,500 km/h, 930 mph)
Range: 1,430 km (772 nmi, 888 mi) with maximum internal fuel
Ferry range: 2,100 km (1,300 mi) with 1 drop tank
Service ceiling: 18,013 m (59,100 ft)
Rate of climb: initial 330 m/s average 109 m/s 06000 m[126] (65,000 ft/min)
Wing loading: 442 kg/m² (90.5 lb/ft²)
Thrust/weight: 1.08
Armament
1 x 30 mm GSh-30-1 cannon with 150 rounds
7 Hard points: 6 x pylons under-wing, 1 x under fuselage
Up to 3,500 kg (7,720 lb) of weapons including six air-to-air missiles a mix of semi-active radar homing (SARH) and AA-8 "Aphid", AA-10 "Alamo", AA-11 "Archer", AA-12 "Adder", FAB 500-M62, FAB-1000, TN-100, ECM Pods, S-24, AS-12, AS-14
Avionics
Phazotron N019, N010 radars
