Hi Mandoble,
>Did it use really MW50 in the third tank?
I don't think the Fw 190A-8 was ever used with MW50. (I could be wrong, though :-)
>If not, was that tank normally used for normal fuel?
Yes. Normal fuel could be injected into the supercharger air intake, though, achieving a similar effect as MW50, raising the boost from 1.42 ata to 1.58/1.65 ata for some extra horsepower. The boosted Fw 190A-8 achieved similar speeds as the Fw 190A-5, and with identical equipment probably came close in climb rate.
>If yes, did the increased range justify the increased weight, decreased acceleration/climb rate and top speed?
Apparently, since the tank was kept in most instances :-)
>If no, why to keep that tank inboard?
It wasn't always kept: The Soviets captured a "light-weight" Fw 190A-8 without outer wing guns, rear fuselage tank, bomb racks etc., and probably without the radio equipment necessary in the home defense. It had just below 4000 kg, about what the A-5 weighed, too.
>The schematic drawings of 190A8 featuring GM-1 show a single big pressurized bottle instead of the aux fuel tank, very different in shape. That bottle was much bigger than those used in pairs by the 109s.
The final form of GM-1 usage in the Me 109 consisted of a single pressure vessel just like the one you describe for the Fw 190. I think before its introduction, smaller vessels were used in quadruples, not in pairs though.
>About the usefullness of GM-1 in the 190A8 it depends on the performance improvements above 22k, where they needed to intercept the buff formations.
The chart Furious posted indicates that GM-1 could be used from 8 km up. The RPM reduction does not necessarily indicate a heat problem - remember that GM-1 provides additional oxygen without the need to spin the supercharger as fast as possible, so a lower RPM setting might as well indicate a new optimum operating point for the engine with less power used for operating the supercharger. Maybe the increased propeller efficiency at lower Mach numbers also plays a role.
Still, it's true that GM-1 use seems to have been limited by thermal considerations. GM-1 provides the same amount of power at sea level as it does at altitude, and it could have provided 250 HP as low as 2 km without mechanically overstressing the engine.
Regards,
Henning (HoHun)