Rumors PAK-FA uses prototype 117 (not 117S) engines for its first flight. Most likely these 117 engines will be installed on first serial PAK-FA as true 5-gen egines will not be ready by 2015.
Even 117 engines said to provide enough thrust for superuise, although not in optimal manner.
More thrust needed for supercruise without afterburner, this will actually reduce fuel consumtion.
Thrust isn't all that important for speed.
As an example, F100 engine equipped F-16's are barely able to make M2.0.
J79 engine equipped F-16's for Taiwan hit M2.05 at times and could have gone faster but the airframe wasn't cleared for it. Yet the F100 far exceeded the thrust output of the J79:
F100 - 22,000lbs of thrust (maximum in reheat).
J79 - 17,500lbs of thrust (maximum in reheat).
Why is this relevant? F100 makes much greater thrust than the J79 as shown, but the J79 is optimised for top end speed and maintains it's thrust better as the mach number rises because it had a much higher exhaust velocity.
High exhaust velocity is the best way to ensure a supercruise capability, but it usually infers other issues with the engine. The J79 for instance is a turbojet whereas the F100 is a turbofan.
The F100 is a far more economical and reliable engine for the majority of flight regimes than the J79. Acceleration and engine economy (both in fuel consumption and reliability and support cost) is also mostly far more useful for a fighter than outright performance.
Furthermore engines such as the F119 which ARE optimised for supercruising (ie: non-reheat) supersonic cruise performance generally provide pretty sucky subsonic performance and fuel consumption (SFC) and this has a great effect on aircraft designed for deep penetration strike missions.
So when some well-known but not well regarded commentators start boasting about PAK-FA being such a high performer AND boast such a long range, in an aircraft package no bigger than existing Flanker models, well one has to take these claims with a very large grain of salt.
Unless Russia has made engine technology leaps that dwarf what anyone else in the world has ever been able to achieve, then these claims are simply bogus.
Supercruising does not use the fuel that reheat function does on supersonic "dash" fighters I agree, but it DOES impose range penalties on an aircraft, which is why the F-22 being such a relatively large fighter has such a relatively poor combat range and why the F-35 WILL be superior in range to the F-22. Supercruising doesn't burn fuel like reheat, but it DOES burn far more than economical subsonic cruising...
It also explains why supercruising Concorde jets existed in the 70's but subsonic jetliners STILL dominate the market today and the Concorde is gone. The cost of a true supercruising capability in fuel and development is NOT trivial...
I find it equally implausible that any OTHER aircraft will achieve differently in the near future either...