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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? |
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