Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Focke-Wulf Ta 152H-1 Single-Seat, Single-Engine High-Altitude Fighter-Interceptor Aircraft.
1 x Junkers Jumo 213E-3 12-cylinder liquid cooled V-type engine developing 1,750 horsepower and driving a three-bladed propeller unit at the nose.
Propulsion
472 mph
759 kph | 410 kts
Max Speed
48,556 ft
14,800 m | 9 miles
Service Ceiling
1,243 miles
2,000 km | 1,080 nm
Operational Range
3,445 ft/min
1,050 m/min
Rate-of-Climb