Sukhoi PAK FA (T-50) Stealth Air Superiority Fighter - Russian Air Force [Review] HD

We are sure, that all the fans of Military Weapons will find here something related to their interests. Subscribe ✈✈✈ https://goo.gl/pY8ZSL ✈✈✈ Remember that these are not toys :) ---------------------------------------------------------- Our Social Media: Facebook - https://goo.gl/4qiHyZ Google+ - https://goo.gl/vq7COr Twitter - https://goo.gl/ueKTdP Taringa - https://goo.gl/jwrjpZ ---------------------------------------------------------- Best Fighter Jets || Military Weapons https://goo.gl/vyby9h ---------------------------------------------------------- Music Info: Demilitarized Zone - Ethan Meixsell ----------------------------------------------------------------------------------------------------------- The Sukhoi PAK FA is a fifth-generation fighter programme of the Russian Air Force. The T-50 is the name of the prototype aircraft designed by Sukhoi for the PAK FA programme. The aircraft is a stealthy, single-seat, twin-engine jet fighter, and will be the first operational aircraft in Russian service to use stealth technology. It is a multirole fighter designed for air superiority and attack roles. The fighter is planned to have supercruise, stealth, supermaneuverability, and advanced avionics to overcome the prior generation of fighter aircraft as well as ground and maritime defences. Role: Stealth Air superiority fighter National origin: Russia Design group: Sukhoi Built by: KnAAPO, NAPO First flight: 29 January 2010 Introduction: 2018 (planned) Status: Final flight testing/pre-production Primary users: Russian Air Force, Russian Navy Produced: 2009–present Number built: 6 flyable prototypes Program cost: US$8–10 billion Unit cost: T-50: US$50+ million Variants: Sukhoi/HAL FGFA Crew: 1 Length: 19.8 m Wingspan: 13.95 m Height: 4.74 m Wing area: 78.8 m2 Empty weight: 18,000 kg Loaded weight: 25,000 kg typical mission weight, 29,270 kg at full load Max. takeoff weight: 35,000 kg Powerplant: 2 × NPO Saturn izdeliye 117 (AL-41F1) for initial production, izdeliye 30 for later production thrust vectoring turbofan Dry thrust: 93.1 kN / 107 kN each Thrust with afterburner: 147 kN / 167 kN each Fuel capacity: 10,300 kg Maximum speed: At altitude: Mach 2.0 (2,140 km/h) Supercruise: Mach 1.6 (1,700 km/h) Range: 3,500 km subsonic 1,500 km supersonic Ferry range: 5,500 km Service ceiling: 20,000 m Wing loading: 317–444 kg/m2 Thrust/weight: Saturn 117: 1.02 (1.19 at typical mission weight) izdeliye 30: 1.16 (1.36 at typical mission weight) Maximum g-load: +9.0 g Guns: 1× 30 mm (1.181 in) 9A1-4071K (GSh-301) cannon in right LEVCON root Air to air loadout: 4× K-77M or 4× izdeliye 810 2× K-74M2 or 2× izdeliye 300 Air to ground loadout: 4× Kh-38M or 4× Kh-58UShK or 8× KAB-250 or 4× KAB-500 2× K-74M2 or 2× izdeliye 300 Air to sea loadout: 4× Kh-35 2× K-74M2 or 2× izdeliye 300 Hardpoints: Six external hardpoints. Kh-31 R-73 R-77