Abro este post para que entre todos compartamos información de lo que supuestamente será el avión de 5º generación ruso y de esta manera armamos algo entre todos
Acá dejo lo que pude encontrar de este esquivo proyecto
General characteristics
* Crew: 1 (pilot)
* Length: 22.0 m (72 ft 2 in)
* Wingspan: 14.2 m (46 ft 7 in)
* Height: 6.05 m (19 ft 10 in)
* Wing area: 78.8 m² (848 ft²)
* Empty weight: 18,500 kg (40,786 lb)
* Loaded weight: 26,000 kg (57,320 lb)
* Useful load: 7,500 kg (16,535 lb)
* Max takeoff weight: 37,000 kg (81,571 lb)
* Powerplant: 2× Saturn-Lyulka AL-41F turbofan
o Dry thrust: 9,800 kgf (21,605 lbf) each
o Thrust with afterburner: 15,500 kgf (34,172 lbf) each
Performance
* Maximum speed: Mach 2.5 at altitude (2,527 km/h, 1,586 mph)
* g-limits: +10 to +11 g (+98.1 to +107.9 m/s², +321.7 to +353.9 ft/s²)
* Cruise speed: 1,300 km/h (807.8 mph)
* Ferry range: 4,000 to 5,500 km (2,485 to 3,418 mi)
* Service ceiling 20,000 m (65,617 ft)
* Rate of climb: 350 m/s (68,898 ft/min)
* Wing loading: 470 kg/m² (96.3 lb/ft²)
* Thrust/weight: 0.84 (dry thrust)
* Minimum thrust/weight:
o With afterburner: 1.19
* Runway length requirement: 350 m (1,148 ft)
* Endurance: 3.3 hrs (198 mins)
Armament
* Guns: 2× 30 mm internal cannon
* Hardpoints: 8 total, 4 on each side of the aircraft.
Avionics
* Radar: N050(?)BRLS AESA/PESA Radar (Enhancement of IRBIS-E) on SU-35
o Frequency: 3 mm (0.118 in)
o Diameter: 0.7 m (2 ft 4 in)
o Targets: 32 tracked, 8 engaged
o Range: 400 km (248 mi)
+ EPR: 3 m² (32.3 ft²) at 160 km (99.4 mi)
+ RCS: 0.01 m² at 90 km (55 mi)
+ Azimuth: +/-70°, +90/-50°
o Power: 4,000 W
o Weight: 65 to 80 kg (143 to 176 lb)
Este seria una de sus posibles aspectos
Esta es una ilustración que salió en una revista india
Tengan en cuenta que este país será uno de los benefactores del proyecto de este avión de 5º generación.
Acá dejo lo que pude encontrar de este esquivo proyecto
General characteristics
* Crew: 1 (pilot)
* Length: 22.0 m (72 ft 2 in)
* Wingspan: 14.2 m (46 ft 7 in)
* Height: 6.05 m (19 ft 10 in)
* Wing area: 78.8 m² (848 ft²)
* Empty weight: 18,500 kg (40,786 lb)
* Loaded weight: 26,000 kg (57,320 lb)
* Useful load: 7,500 kg (16,535 lb)
* Max takeoff weight: 37,000 kg (81,571 lb)
* Powerplant: 2× Saturn-Lyulka AL-41F turbofan
o Dry thrust: 9,800 kgf (21,605 lbf) each
o Thrust with afterburner: 15,500 kgf (34,172 lbf) each
Performance
* Maximum speed: Mach 2.5 at altitude (2,527 km/h, 1,586 mph)
* g-limits: +10 to +11 g (+98.1 to +107.9 m/s², +321.7 to +353.9 ft/s²)
* Cruise speed: 1,300 km/h (807.8 mph)
* Ferry range: 4,000 to 5,500 km (2,485 to 3,418 mi)
* Service ceiling 20,000 m (65,617 ft)
* Rate of climb: 350 m/s (68,898 ft/min)
* Wing loading: 470 kg/m² (96.3 lb/ft²)
* Thrust/weight: 0.84 (dry thrust)
* Minimum thrust/weight:
o With afterburner: 1.19
* Runway length requirement: 350 m (1,148 ft)
* Endurance: 3.3 hrs (198 mins)
Armament
* Guns: 2× 30 mm internal cannon
* Hardpoints: 8 total, 4 on each side of the aircraft.
Avionics
* Radar: N050(?)BRLS AESA/PESA Radar (Enhancement of IRBIS-E) on SU-35
o Frequency: 3 mm (0.118 in)
o Diameter: 0.7 m (2 ft 4 in)
o Targets: 32 tracked, 8 engaged
o Range: 400 km (248 mi)
+ EPR: 3 m² (32.3 ft²) at 160 km (99.4 mi)
+ RCS: 0.01 m² at 90 km (55 mi)
+ Azimuth: +/-70°, +90/-50°
o Power: 4,000 W
o Weight: 65 to 80 kg (143 to 176 lb)
Este seria una de sus posibles aspectos
Esta es una ilustración que salió en una revista india
Tengan en cuenta que este país será uno de los benefactores del proyecto de este avión de 5º generación.