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Sukhoi PAK FA

PAK FA
PAK FA T-50 prototype on the day of its first flight
Role	Stealth multirole fighter
National origin	Russia
Manufacturer	Sukhoi
First flight	January 29, 2010
Introduction	2013 (planned)
Status	Test flight / Pre-production
Primary user	Russian Air Force
Number built	3
Program cost	US$8-10 billion (est.)
Unit cost	US$100 million (est.)
Variants	Sukhoi/HAL FGFA

Specifications

Because the aircraft is in development, these specifications are preliminary and are taken as estimates from the available images.

Data from 

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)
• Powerplant: 2× New unnamed engine by NPO Saturn and FNPTS MMPP Salyut of 175 kN each. Prototype with AL-41F1 of 147 kN each, definitive version with new engine >157 kN
• Maximum Fuel weight: 10,300 kg (22,711 lb)

Performance

• Maximum speed: 2,600 km/h (Mach 2.45) (at 17,000 m altitude) (1,615 mph (at 45,000 ft altitude))
• Cruise speed: 1,300 - 1,800 km/h (808 - 1,118 mph)
• Ferry range: 5,500 km ()
• Service ceiling: 20,000 m (65,616 ft)
• Rate of climb: 350 m/sec (1184 ft/sec)
• Wing loading: 330(normal) - 470(maximum) kg/m² (67(normal) - 96(maximum) lb/ft²)
• Thrust/weight: 1.4
• Maximum g-load: +10.0/+11.0 g 

Armament

• Guns: None on prototype. Apparent provision for a cannon (Most likely GSh-301)
• Hardpoints: Two internal bays estimated at 4.6-4.7 metres by 1-1.1 metres. Other sources suggest two auxiliary internal bays for short range AAMS and 6 external hardpoints

Avionics

N050(?)BRLS AFAR/AESA built by Tikhomirov NIIP and based on Tikhomirov NIIP N035 Irbis-E.

It will be the second aircraft based AESA Radar to be built by Russia, the first being the Phazotron NIIR ZHUK-A Radar in the MIG-35.

Designed armament

Two Izdeliye 810 Extended beyond visual range missiles per weapons bay. Multiple Izdeliye 180 / K77M beyond visual range missiles. K74 and K30 within visual range missiles can also be carried.

Two KH38M or KH58 USHK air-to-ground missiles per weapons bay.

Multiple 250-500kg precision guided bombs per weapons bay, with a maximum of ten bombs in internal bays.

Other possible loads include one 1500kg bomb per weapons bay or two 400km+ range anti-AWACS weapons on external hard-points. A maximum weapons load of 7500kg is reported.

Comparison

Comparison of performance of fifth generation jet fighter

	Maximum speed:	Supercruise:	Ferry Range (max):	Service ceiling:	RCS:
F-35:	2,065 km/h (1,283 mph) - Mach 1.67	No data	2,220 km	18,288 m (60,000 ft)	0.0015 m^2
F-22:	2,410 km/h (1,500 mph) - Mach 2.25	1,963 km/h (1,220 mph)	2,960 km	19,812 m (65,000 ft)	0.0002 m^2
T-50:	2,600 km/h (1,615 mph) - Mach 2.45	1,800 km/h (1,118 mph)	5,500 km	20,000 m (65,616 ft)	0.5 m^2

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