Teh One Who Knocks
11-26-2012, 04:34 PM
http://i.imgbox.com/acbwItwu.jpg (http://imgbox.com/acbwItwu)
The Sukhoi PAK FA is a twin-engine jet fighter being developed by Sukhoi for the Russian Air Force. The Sukhoi T-50 is the prototype for PAK FA.
The first flight of the PAK FA was performed on 29th of January, 2010. The serial production is expected to start in 2015.
http://i.imgbox.com/adx3HgB8.jpg (http://imgbox.com/adx3HgB8)
The plane was designed to replace Su-27 for the Russian Air Forces. They are also developing an export modification together with India, it is called FGFA – Fifth Generation Fighter Aircraft.
http://i.imgbox.com/abs9yYgr.jpg (http://imgbox.com/abs9yYgr)
The plane is expected to be 2,5-3 times cheaper than its foreign analogues.
India plans to buy PAK FA for 100 million dollars per one.
http://i.imgbox.com/acwzgxiR.jpg (http://imgbox.com/acwzgxiR)
On its first flights, the PAK FA was expected to use a pair of conventional Saturn 117S engines, but it was a new engine 117 (AL-41F1) that powered its first flight. It’s a turbofan engine with an afterburner and thrust vector control.
The engine enables to develop supersonic speed without use of an afterburner, it also has a fully digital control system and a plasma ignition system.
http://i.imgbox.com/abs3NMJE.jpg (http://imgbox.com/abs3NMJE)
The PAK FA has a reported maximum weapons load of 7,500 kg (16534 lb). It has an apparent provision for a cannon (most likely GSh-301), and could possibly carry two 30 mm cannons.
http://i.imgbox.com/acmppqGG.jpg (http://imgbox.com/acmppqGG)
The integrated multi-function radar system of the PAK FA will contain 5 internal antennas.
http://i.imgbox.com/abpuULd0.jpg (http://imgbox.com/abpuULd0)
The PAK FA will be equipped with 1526 transceiver modules which will provide a greater detection range, multichannel tracking of targets and an ability to use guided missile weapons for their destruction.
http://i.imgbox.com/adtF2riF.jpg (http://imgbox.com/adtF2riF)
An extra radar station will allow to increase noise immunity and combat survivability, and neautralize technologies of reducing aircrafts visibility used by an opponent.
http://i.imgbox.com/adxkZ7mU.jpg (http://imgbox.com/adxkZ7mU)
The visibility of T-50 is also reduced by its shape, materials absorbing and reflecting radio waves and materials which are used for the air frame coating.
http://i.imgbox.com/acfBNKj6.jpg (http://imgbox.com/acfBNKj6)
General characteristics:
Crew: 1
Length: 19.8 m (65.9 ft)
Wingspan: 14 m (46.6 ft)
Height: 6.05 m (19.8 ft)
Wing area: 78.8 m2 (848.1 ft2)
Empty weight: 18,500 kg (40,785 lb)
Loaded weight: 26,000 kg (57,320 lb)
Useful load: 7,500 kg (combat load) (16,534 lb)
Max. takeoff weight: 37,000 kg (81,570 lb)
Fuel capability: 10,300 kg (22,711 lb)[100]
Performance:
Maximum speed: Mach 2+, 2,100-2,600 km/h (1,300-1,560 mph) ; at 17,000 m (45,000 ft) altitude
Cruise speed: 1,300-1,800 km/h[102] (808-1,118 mph)
Ferry range: 5,500 km[64] (3,417 mi)
Service ceiling: 20,000 m (65,600 ft)
Rate of climb: 350 m/s (68,900 ft/min)
Wing loading: 330-470 kg/m2 (67-96 lb/ft2)
http://i.imgbox.com/addgeiBa.jpg (http://imgbox.com/addgeiBa)
http://i.imgbox.com/acrMnpek.jpg (http://imgbox.com/acrMnpek)
http://i.imgbox.com/acs2s0xE.jpg (http://imgbox.com/acs2s0xE)
The Sukhoi PAK FA is a twin-engine jet fighter being developed by Sukhoi for the Russian Air Force. The Sukhoi T-50 is the prototype for PAK FA.
The first flight of the PAK FA was performed on 29th of January, 2010. The serial production is expected to start in 2015.
http://i.imgbox.com/adx3HgB8.jpg (http://imgbox.com/adx3HgB8)
The plane was designed to replace Su-27 for the Russian Air Forces. They are also developing an export modification together with India, it is called FGFA – Fifth Generation Fighter Aircraft.
http://i.imgbox.com/abs9yYgr.jpg (http://imgbox.com/abs9yYgr)
The plane is expected to be 2,5-3 times cheaper than its foreign analogues.
India plans to buy PAK FA for 100 million dollars per one.
http://i.imgbox.com/acwzgxiR.jpg (http://imgbox.com/acwzgxiR)
On its first flights, the PAK FA was expected to use a pair of conventional Saturn 117S engines, but it was a new engine 117 (AL-41F1) that powered its first flight. It’s a turbofan engine with an afterburner and thrust vector control.
The engine enables to develop supersonic speed without use of an afterburner, it also has a fully digital control system and a plasma ignition system.
http://i.imgbox.com/abs3NMJE.jpg (http://imgbox.com/abs3NMJE)
The PAK FA has a reported maximum weapons load of 7,500 kg (16534 lb). It has an apparent provision for a cannon (most likely GSh-301), and could possibly carry two 30 mm cannons.
http://i.imgbox.com/acmppqGG.jpg (http://imgbox.com/acmppqGG)
The integrated multi-function radar system of the PAK FA will contain 5 internal antennas.
http://i.imgbox.com/abpuULd0.jpg (http://imgbox.com/abpuULd0)
The PAK FA will be equipped with 1526 transceiver modules which will provide a greater detection range, multichannel tracking of targets and an ability to use guided missile weapons for their destruction.
http://i.imgbox.com/adtF2riF.jpg (http://imgbox.com/adtF2riF)
An extra radar station will allow to increase noise immunity and combat survivability, and neautralize technologies of reducing aircrafts visibility used by an opponent.
http://i.imgbox.com/adxkZ7mU.jpg (http://imgbox.com/adxkZ7mU)
The visibility of T-50 is also reduced by its shape, materials absorbing and reflecting radio waves and materials which are used for the air frame coating.
http://i.imgbox.com/acfBNKj6.jpg (http://imgbox.com/acfBNKj6)
General characteristics:
Crew: 1
Length: 19.8 m (65.9 ft)
Wingspan: 14 m (46.6 ft)
Height: 6.05 m (19.8 ft)
Wing area: 78.8 m2 (848.1 ft2)
Empty weight: 18,500 kg (40,785 lb)
Loaded weight: 26,000 kg (57,320 lb)
Useful load: 7,500 kg (combat load) (16,534 lb)
Max. takeoff weight: 37,000 kg (81,570 lb)
Fuel capability: 10,300 kg (22,711 lb)[100]
Performance:
Maximum speed: Mach 2+, 2,100-2,600 km/h (1,300-1,560 mph) ; at 17,000 m (45,000 ft) altitude
Cruise speed: 1,300-1,800 km/h[102] (808-1,118 mph)
Ferry range: 5,500 km[64] (3,417 mi)
Service ceiling: 20,000 m (65,600 ft)
Rate of climb: 350 m/s (68,900 ft/min)
Wing loading: 330-470 kg/m2 (67-96 lb/ft2)
http://i.imgbox.com/addgeiBa.jpg (http://imgbox.com/addgeiBa)
http://i.imgbox.com/acrMnpek.jpg (http://imgbox.com/acrMnpek)
http://i.imgbox.com/acs2s0xE.jpg (http://imgbox.com/acs2s0xE)