For the experts:

As made obvious by its wings, the Ta-152H was designed as a
high-altitude interceptor. But I am interested in how the Ta-152H
handled at low-to-medium altitudes. How did the Ta-152H compare with
the Fw-190D at such alts? I suppose the ultra-long wings of the Ta
considerably reduced rollrate? Did the Ta have increased
manuverability/tighter turning circle at low alts? (Was wing-loading
increased or decreased?) What about low-speed & stall characteristics?