Indicated stall speed in flight configuration: 150..184 km/h
Indicated stall speed in takeoff/landing configuration: 123..151 km/h
Dive speed limit: 560 km/h
Maximum load factor: 4.5 G
Stall angle of attack in flight configuration: 20 °
Stall angle of attack in landing configuration: 17 °
Maximum true air speed at sea level, engine mode - Climb: 369 km/h
Maximum true air speed at 2000 m, engine mode - Climb: 398 km/h
Maximum true air speed at 5000 m, engine mode - Climb: 405 km/h
Service ceiling: 6300 m
Climb rate at sea level: 4.5 m/s
Climb rate at 3000 m: 3.6 m/s
Climb rate at 6000 m: 1.8 m/s
Maximum performance turn at sea level: 30.8 s, at 250 km/h IAS.
Maximum performance turn at 3000 m: 45.2 s, at 250 km/h IAS.
Flight endurance at 3000 m: 8.5 h, at 300 km/h IAS.
Takeoff speed: 170..210 km/h
Glideslope speed: 180..200 km/h
Landing speed: 125..150 km/h
Landing angle: 9 °
Note 1: the data provided is for international standard atmosphere (ISA).
Note 2: flight performance ranges are given for possible aircraft mass ranges.
Note 3: maximum speeds, climb rates and turn times are given for standard aircraft mass.
Note 4: climb rates are given for Climb power, turn times are given for Take-off power.
Engine:
Model: Jumo-211J
Maximum power in Take-off mode at sea level: 1420 HP
Maximum power in Climb mode at sea level: 1190 HP
Maximum power in Climb mode at 1500 m: 1260 HP
Maximum power in Climb mode at 4900 m: 1180 HP
Engine modes:
Nominal (unlimited time): 2250 RPM, 1.15 ata
Climb power (up to 30 minutes): 2400 RPM, 1.25 ata
Take-off power (up to 1 minute): 2600 RPM, 1.42 ata
Water rated temperature in engine output: 80 °C
Water maximum temperature in engine output: 110 °C
Oil rated temperature in engine output: 90 °C
Oil maximum temperature in engine output: 105 °C
Supercharger gear shift altitude: automatic
Empty weight: 8963 kg
Minimum weight (no ammo, 10% fuel): 9946 kg
Standard weight: 13727 kg
Maximum takeoff weight: 15239 kg
Fuel load: 3214 kg / 4285 l
Useful load: 6276 kg
Defensive armament:
Nose: 7.92mm machine gun "MG 15", 600 rounds, 1000 rounds per minute
Top: 7.92mm machine gun "MG 15", 1125 rounds, 1000 rounds per minute
Belly-backward: 7.92mm machine gun "MG 15", 1200 rounds, 1000 rounds per minute
Belly-forward: 7.92mm machine gun "MG 15", 675 rounds, 1000 rounds per minute
Left: 7.92mm machine gun "MG 15", 450 rounds, 1000 rounds per minute
Right: 7.92mm machine gun "MG 15", 450 rounds, 1000 rounds per minute
Nose: 20mm gun "MG FF", 240 rounds, 540 rounds per minute (modification)
Belly-forward: 20mm gun "MG FF", 330 rounds, 540 rounds per minute (modification)
Bombs:
Up to 16 x 55 kg general purpose bombs "SC 50"
Up to 4 x 249 kg general purpose bombs "SC 250"
500 kg general purpose bomb "SC 500"
Up to 2 x 1090 kg general purpose bombs "SC 1000"
Up to 2 x 1780 kg general purpose bombs "SC 1800"
2400 kg general purpose bomb "SC 2500"
Length: 16.38 m
Wingspan: 22.5 m
Wing surface: 79.5 m^2
Combat debut: June 1941
Additional Configurations[ | ]
2 x 1090 kg General Purpose Bomb SC 1000
Additional mass: 2180 kg
Ammunition mass: 2180 kg
Estimated speed loss before drop: 23 km/h
Estimated speed loss after drop: 0 km/h
2 x 1780 kg General Purpose Bomb SC 1800
Additional mass: 3560 kg
Ammunition mass: 3560 kg
Estimated speed loss before drop: 32 km/h
Estimated speed loss after drop: 0 km/h
2400 kg General Purpose Bomb SC 2500
Additional mass: 2400 kg
Ammunition mass: 2400 kg
Estimated speed loss before drop: 17 km/h
Estimated speed loss after drop: 0 km/h
Nose turret with 20mm MG FF gun with 240 rounds
Additional mass: 46 kg
Estimated speed loss: 0 km/h
Belly forward-looking turret with 20mm MG FF gun with 300 rounds
Additional mass: 147 kg
Estimated speed loss: 0 km/h
