Mig-35 offered to India matches all requirements: Russia

Press Trust Of India
Moscow, July 26, 201


Russia on Monday said that its new Mig-35 fighter had passed Indian Air Forces three evaluation tests and matched all requirements listed by New Delhi in the $10 billion tender for 126 medium multi-role combat aircraft (MMRCA). "The requirements of the tender are quite rigid, but we have already held three valuation tests, and we believe we have offered an aircraft which entirely corresponds to the tender requirements," a senior official of the Rosoboronexport State Corporation Sergei Kornyev said.

His comments come as India is believed to be in the process of shortlisting the bidders.

Major aircraft manufacturers including the French Dassault Aviation with its Rafale jet fighter, US Lockheed Martin with its F-16 Falcon and Boeing with F-18 Super Hornet, the Swedish Saab with its most up-to-date Gripen fighter and Eurofighter are in the fray along with MiG-35 Fulcrum-F.

More:http://www.hindustantimes.com/Mig-35-offered-to-India-matches-all-requirements-Russia/Article1-577956.aspx

Lockheed Martin F-22 Raptor

This two picture are taken from http://www.aircraft-wallpaper.com/

F-22- Raptor- ,take-off-stealth

From Wikipedia, the free encyclopedia
The Lockheed Martin/Boeing F-22 Raptor is a single-seat, twin-engine fifth-generation fighter aircraft that uses stealth technology. It was designed primarily as an air superiority fighter, but has additional capabilities that include ground attack, electronic warfare, and signals intelligence roles.

1. 
   

General characteristics

• Crew: 1
• Length: 62 ft 1 in (18.90 m)
• Wingspan: 44 ft 6 in (13.56 m)
• Height: 16 ft 8 in (5.08 m)
• Wing area: 840 ft² (78.04 m²)
• Airfoil: NACA 64A?05.92 root, NACA 64A?04.29 tip
• Empty weight: 43,430 lb (19,700 kg^[2][189])
• Loaded weight: 64,460 lb (29,300 kg^[190])
• Max takeoff weight: 83,500 lb (38,000 kg)
• Powerplant: 2× Pratt & Whitney F119-PW-100 Pitch Thrust vectoring turbofans
  
  • Dry thrust: 23,500 lb^[191] (104 kN) each
  • Thrust with afterburner: 35,000+ lb^[2][191] (156+ kN) each
• Fuel capacity: 18,000 lb (8,200 kg) internally,^[2][189] or 26,000 lb (11,900 kg) with two external fuel tanks^[2][189]

Performance

• Maximum speed:
  
  
  • At altitude: Mach 2.25 (1,500 mph, 2,410 km/h)^[90]
  • Supercruise: Mach 1.82 (1,220 mph, 1,963 km/h)^[90]
• Range: 1,600 nmi (1,840 mi, 2,960 km) with 2 external fuel tanks
• Combat radius: 410 nmi^[188] (471 mi, 759 km)
• Ferry range: 2,000 mi (1,738 nmi, 3,219 km)
• Service ceiling: 65,000 ft (19,812 m)
• Wing loading: 77 lb/ft² (375 kg/m²)
• Thrust/weight: 1.08 (1.26 with loaded weight & 50% fuel)
• Maximum design g-load: -3.0/+9.0 ^[90]