Hi Widewing,
>There's a fellow on another BBS who insists that he has data showing the Ta 152H-1 was capable of 500+ mph.
I have never heard of that. If he actually has data, I'd like to see it, too :-)
>To attain 500 mph the 152 would require at least 3,000 hp, perhaps even more.
Of course, the power requirement would be highly altitude-dependend. Using Wilbus' figure of 472 mph @ 41000 ft as standard top speed, it's achieved on just 1080 hp (plus a considerable amount of exhaust thrust).
To get to 500 mph, or 106% of the original speed, you'd just have to produce 118% of the original power, or 1280 hp. Since the original power is achieved on 120 g/s GM-1 injection and the GM-1 system will yield a maximum of 180 g/s, this power increase is well in reach for the Jumo 213E.
However, 180 g/s is only cleared for 42650 ft and above, and I believe you might end up melting important parts of your engines if you engage it below that while aiming for the 500 mph mark :-)
There are possible explanations how a Ta 152H could have been flown at 500 mph - experimental engine, prototype with low fuel load and without combat equipment, or - maybe the highest probability guess - an airspeed reading not corrected for compressiblity error :-)
(The compressibilty error at the speed and altitude Wilbus mentioned would read about 50 mph too high in a conventional airspeed indicator. I don't know if the Ta 152 maybe had the late-war "jet fighter" type airspeed indicator which had a IAS gauge for low speeds and a TAS gauge for higher speeds, but I suspect the TAS gauge might not have compensated for compressiblity either.)
I agree that such a record flight would probably have been mentioned in the extensive literature on the type, and in the absence of data I'd consider the 500 mph claim as plain wishful thinking :-)
Regards,
Henning (HoHun)