He 111 H-6

He 111 H-6 is a German bomber available as part of Battle of Stalingrad.

Specifications
 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