Responder al tema

Mensaje

<blockquote data-quote="HANO_DEINOVITZ" data-source="post: 465670" data-attributes="member: 3601">Abro este post&nbsp; para que entre todos compartamos información de lo que supuestamente será el avión de 5º generación ruso&nbsp; y de esta manera armamos algo entre todos Acá dejo&nbsp; lo que pude encontrar de este esquivo proyecto General characteristics&nbsp; &nbsp; * Crew: 1 (pilot)&nbsp; &nbsp; * Length: 22.0 m (72 ft 2 in)&nbsp; &nbsp; * Wingspan: 14.2 m (46 ft 7 in)&nbsp; &nbsp; * Height: 6.05 m (19 ft 10 in)&nbsp; &nbsp; * Wing area: 78.8 m² (848 ft²)&nbsp; &nbsp; * Empty weight: 18,500 kg (40,786 lb)&nbsp; &nbsp; * Loaded weight: 26,000 kg (57,320 lb)&nbsp; &nbsp; * Useful load: 7,500 kg (16,535 lb)&nbsp; &nbsp; * Max takeoff weight: 37,000 kg (81,571 lb)&nbsp; &nbsp; * Powerplant: 2× Saturn-Lyulka AL-41F turbofan&nbsp; &nbsp; &nbsp; &nbsp; &nbsp; o Dry thrust: 9,800 kgf (21,605 lbf) each&nbsp; &nbsp; &nbsp; &nbsp; &nbsp; o Thrust with afterburner: 15,500 kgf (34,172 lbf) eachPerformance&nbsp; &nbsp; * Maximum speed: Mach 2.5 at altitude (2,527 km/h, 1,586 mph)&nbsp; &nbsp; * g-limits: +10 to +11 g (+98.1 to +107.9 m/s², +321.7 to +353.9 ft/s²)&nbsp; &nbsp; * Cruise speed: 1,300 km/h (807.8 mph)&nbsp; &nbsp; * Ferry range: 4,000 to 5,500 km (2,485 to 3,418 mi)&nbsp; &nbsp; * Service ceiling 20,000 m (65,617 ft)&nbsp; &nbsp; * Rate of climb: 350 m/s (68,898 ft/min)&nbsp; &nbsp; * Wing loading: 470 kg/m² (96.3 lb/ft²)&nbsp; &nbsp; * Thrust/weight: 0.84 (dry thrust)&nbsp; &nbsp; * Minimum thrust/weight:&nbsp; &nbsp; &nbsp; &nbsp; &nbsp; o With afterburner: 1.19&nbsp; &nbsp; * Runway length requirement: 350 m (1,148 ft)&nbsp; &nbsp; * Endurance: 3.3 hrs (198 mins)Armament&nbsp; &nbsp; * Guns: 2× 30 mm internal cannon&nbsp; &nbsp; * Hardpoints: 8 total, 4 on each side of the aircraft.Avionics&nbsp; &nbsp; * Radar: N050(?)BRLS AESA/PESA Radar (Enhancement of IRBIS-E) on SU-35&nbsp; &nbsp; &nbsp; &nbsp; &nbsp; o Frequency: 3 mm (0.118 in)&nbsp; &nbsp; &nbsp; &nbsp; &nbsp; o Diameter: 0.7 m (2 ft 4 in)&nbsp; &nbsp; &nbsp; &nbsp; &nbsp; o Targets: 32 tracked, 8 engaged&nbsp; &nbsp; &nbsp; &nbsp; &nbsp; o Range: 400 km (248 mi)&nbsp; &nbsp; &nbsp; &nbsp; &nbsp; &nbsp; &nbsp; &nbsp; + EPR: 3 m² (32.3 ft²) at 160 km (99.4 mi)&nbsp; &nbsp; &nbsp; &nbsp; &nbsp; &nbsp; &nbsp; &nbsp; + RCS: 0.01 m² at 90 km (55 mi)&nbsp; &nbsp; &nbsp; &nbsp; &nbsp; &nbsp; &nbsp; &nbsp; + Azimuth: +/-70°, +90/-50°&nbsp; &nbsp; &nbsp; &nbsp; &nbsp; o Power: 4,000 W&nbsp; &nbsp; &nbsp; &nbsp; &nbsp; o Weight: 65 to 80 kg (143 to 176 lb)Este seria una de sus posibles aspectos&nbsp;&nbsp; <img src="http://upload.wikimedia.org/wikipedia/en/thumb/c/cf/Protoype.jpg/453px-Protoype.jpg" alt="" class="fr-fic fr-dii fr-draggable " style="" />Esta es una ilustración que salió en una revista india Tengan en cuenta que este país será uno de los benefactores del proyecto&nbsp; de este avión de 5º generación.<img src="http://bp1.blogger.com/_WE1irOIooUQ/RyYKc4YG8mI/AAAAAAAAAxA/rtOpOSRgo-g/s400/Sukhoi+T-50+PAK+FA+pakfa_india.jpg" alt="" class="fr-fic fr-dii fr-draggable " style="" /></blockquote>

[QUOTE="HANO_DEINOVITZ, post: 465670, member: 3601"] 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 [B]General characteristics[/B] [COLOR="Red"] * 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 [/COLOR] [B]Performance [/B] * [COLOR="Red"]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) [/COLOR] [B]Armament[/B] *[COLOR="Red"] Guns: 2× 30 mm internal cannon * Hardpoints: 8 total, 4 on each side of the aircraft. [/COLOR] [B]Avionics[/B] [COLOR="Red"] * 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) [/COLOR] Este seria una de sus posibles aspectos [IMG]http://upload.wikimedia.org/wikipedia/en/thumb/c/cf/Protoype.jpg/453px-Protoype.jpg[/IMG] 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. [IMG]http://bp1.blogger.com/_WE1irOIooUQ/RyYKc4YG8mI/AAAAAAAAAxA/rtOpOSRgo-g/s400/Sukhoi+T-50+PAK+FA+pakfa_india.jpg[/IMG] [/QUOTE]

Verificación

Guerra desarrollada entre Argentina y el Reino Unido en 1982