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He 111 H-16

he111h16

Description

Indicated stall speed in flight configuration: 150..194 km/h
Indicated stall speed in takeoff/landing configuration: 123..156 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: 370 km/h
Maximum true air speed at 2000 m, engine mode - Climb: 399 km/h
Maximum true air speed at 5000 m, engine mode - Climb: 410 km/h

Service ceiling: 6850 m
Climb rate at sea level: 5.3 m/s
Climb rate at 3000 m: 4.1 m/s
Climb rate at 6000 m: 2.3 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: 6.7 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-211F
Maximum power in Take-off mode at sea level: 1340 HP
Maximum power in Climb mode at sea level: 1120 HP
Maximum power in Climb mode at 1900 m: 1210 HP
Maximum power in Climb mode at 5300 m: 1060 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, 1.40 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: 8698 kg
Minimum weight (no ammo, 10%25 fuel): 9831 kg
Standard weight: 13017 kg
Maximum takeoff weight: 15689 kg
Fuel load: 2553 kg / 3450 l
Useful load: 6991 kg

Defensive armament:
Nose: 20mm gun “MG FF”, 240 rounds, 540 rounds per minute
Top: 13mm machine gun “MG 131”, 1000 rounds, 900 rounds per minute
Belly-backward: 2 x 7.92mm machine guns “MG 81”, 850 rounds, 1600 rounds per minute
Left: 7.92mm machine gun “MG 81”, 500 rounds, 1600 rounds per minute
Right: 7.92mm machine gun “MG 81”, 500 rounds, 1600 rounds per minute

Bombs:
Up to 16 x 55 kg general purpose bombs “SC 50”
Up to 4 x 249 kg general purpose bombs “SC 250”
Up to 2 x 500 kg general purpose bombs “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 m²

Combat debut: winter 1943

Operation features:

Modifications

2 x SC 1000 heavy bombs
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

SC 2500 heavy bomb
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

2 x SC 1800 heavy bombs
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