I giggled when I saw a member as recently as February this year claim that the T-50 will somehow carry four missiles per bay. Let me give you some facts. The following excerpt is pulled from Wikipedia, and its cited using quite reliable sources (Air International, AviationWeek, flateric and flanker from Secret Projects).
The T-50 has two tandem main internal weapon bays each approximately 4.6 m (15.1 ft) long and 1.0 m (3.3 ft) wide and two small triangular-section weapon bays that protrudes under the fuselage near the wing root.
is developing two ejection launchers for the main bays: the UVKU-50L for missiles weighing up to 300 kg (660 lb) and the UVKU-50U for ordinance weighing up to 700 kg (1,500 lb). The aircraft has an internally mounted 9A1-4071K (
) 30 mm cannon near the right LEVCON root.
There is at most room for three K-77M missiles in each bay, and currently, they only plan on having two of those missiles per bay. While the T-50 is capable of carrying a total of 4 Phoenix-size missiles (two per bay), in terms of quantity the air-to-air loadout of the T-50 will be no more than the F-22.
The T-50 will have little difference from the F-22 in terms of speed performance. The T-50 is limited to Mach 2 due to its materials, and I think the F-22 is also operationally limited at that speed. The T-50 does have greater range due to greater internal fuel capacity. It will also probably have the advantage in maneuverability in pitch and especially in yaw due to LEVCON and canted TVC, but rolling acceleration may be worse because of the bigger inertia from widely spaced engines.
Also, Air Force Brat, do you have the original source about the F-22's sustained g capability? I recall Schwarz saying that the F-22 can
pull]/i] 6g at 50,000 ft, but I don't recall him saying that it will sustain it.