He 111 H-16 / IL-2 Sturmovik: Great Battles
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Bomber
He 111 H-16
History
Specifications

Since the provisions of the Treaty of Versailles prohibited Germany from having an air force, the Germans disguised the development of military aircraft as civilian projects until 1935, but immediately designed passenger aircraft as bombers. One of the machines created this way was the He 111, which turned out to be a good bomber and a mediocre passenger plane. From 1936 to 1941, bombers of the A, B, D, E, J, and P series were produced with engines from Daimler-Benz and Jumo. However, since the DB 601 engine was mainly used in fighter aircraft, parallel to the He 111 P, the He 111H was also produced with Jumo 211 engines.

The next mass production modification of the H-family bombers was the He 111 H-16, which went into serial production in December 1942. The powerplant with Jumo 211F-2 engines was taken from the H-6 and the weapons and armor protection from the H-11. The bombs were mounted inside or outside the fuselage, the latter allowing additional fuel tanks to take up space inside the aircraft. The H-16 retained eight ESAC bomb racks in the bomb bay, although the four left racks could be replaced by an 835-liter tank. ETS 2000 mounts were used for externally suspended bombs. Two SC 250 bombs or 32 SC 50 bombs in cassettes could be carried externally, or four SC 250s in the bomb bay and one SC 1000 on an external mount. The use of R-unit solid propellant launchers mounted under the wing increased the maximum bomb load from 2000 kg to 3000 kg.

The defensive armament consisted of an MG/FF cannon in the nose, the lower forward firing point in the ventral gondola was removed and a 7.92 mm twin MG 81Z machine gun was installed in the rear. A 13.2 mm MG 131 machine gun was installed in the upper firing point to protect the rear hemisphere; the drum-fed MG 17 machine guns in the side windows were replaced by belt-fed MG-81 machine guns.

Field modification kits for the He 111 H-16:
  • H-16/R1: instead of the usual upper firing point, an electrically driven turret for a 13mm MG 131 machine gun was installed;
  • H-16/R2: Glider towing plane with metal towing gear from Weser Flugzeugbau;
  • The H-16/R3 was characterized by additional armor protection and a reduced bomb load, which was placed only inside the fuselage. It had two variants, H-16/R3/U1 and H-16/R3/U2, which differed in the type of bomb rack.

By the middle of the war, German troops were increasingly surrounded. To supply them, they developed the Dobbas unmanned cargo glider, which had the appearance of a very short and thick wing. It had no landing gear and landed on its belly. It could carry food, ammunition, weapons, a motorcycle with a sidecar, or a 75 mm antitank gun. The device was suspended from the H-16's belly bomb rack and released from a low altitude onto soft ground or snow. Tests were carried out, but there is no data on the use of Dobbas at the front.

Some of the He-111 H-16s were converted in 1944 to carry Fi 103 cruise missiles. Launching a missile at night in the direction of a large city at an altitude of 500 m, the probability of a hit was very high. From July 1944 the III. Gruppe of Kampfgeschwader 3 used the H-16 along with other missile carriers to launch missiles at London and Southampton.

From the end of 1942 to the end of 1943, the factories produced 1,155 He-111 H-16 bombers; during the same period, 280 H-6s and 35 H-11s were upgraded to the H-16 variant. Although the He 111 became primarily a transport aircraft in 1943, it was also used quite often as a bomber, especially on the Eastern Front.

1. W. Creen “The Warplanes of the Third Reich”, Galahad Books, 1986

2. “Wings of the Luftwaffe” Translation of V. Green’s book “Combat Aircraft of the Third Reich” by A. Firsov, 1993

3. Materials from the site airwar.ru

4. “Heinkel He 111 Photo Archive” War in the Air No. 102, 2000

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% 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:
- Each engine has a two-stage mechanical supercharger with an automatic switch system that switches gears depending altitude and engine revolutions. It can also be manually switched to first gear.
- Engine mixture control is automatic.
- Engine RPM has an automatic governor and it is maintained at the required RPM corresponding to the governor control lever position. The governor automatically controls the propeller pitch to maintain the required RPM.
- Propellers have a feathering system which should be activated in case of engine damage to reduce drag of the propeller in auto-rotation.
- Water and oil radiator shutter controls are manual. The oil radiator control has five fixed positions.
- The aircraft has trimmers for all flight-controls: pitch, roll and yaw.
- Landing flaps have a hydraulic actuator and they can be extended to any angle up to 60°.
- The aircraft tailwheel rotates freely and does not have a lock. For this reason, it is necessary to confidently and accurately operate the rudder pedals during the takeoff and landing.
- The aircraft has independent left and right hydraulic wheel brake controls. To apply either brake push the upper part of the rudder pedal.
- The aircraft has dedicated fuel gauges for left and right fuel tank groups and there is a switch between the internal and external fuel tank group indicator. In game the fuel indicator switch changes by pressing (RShift+I). Also, the airplane has low fuel warning lights (200 liters) for left and right fuel tank groups.
- The aircraft is equipped with an automatic bomb salvo controller, it allows you to switch between the bomb racks to be released (internal or external) and to switch between different salvo quantities. There is also a controller for a drop delay between each bomb in the salvo.
 
Basic data and recommended positions of the aircraft controls:
1. Starting the engine:
- recommended position of the mixture control lever: auto mixture control
- recommended position of the oil radiator control handle: close
- recommended position of the water radiator control handle: close
- recommended position of the prop pitch control handle: light
- recommended position of the throttle lever: 0%
 
2. Recommended mixture control lever positions for various flight modes: auto mixture control
 
3.1 Recommended positions of the oil radiator control handle for various flight modes:
- takeoff: open 50%
- climb: open 100%
- cruise flight: open 25% (in winter conditions - close if necessary)
- combat: open 50%
 
3.2 Recommended positions of the water radiator control handle for various flight modes:
- takeoff: open 50%
- climb: open 100%
- cruise flight: open 20% (in winter conditions - close if necessary)
- combat: open 50%
 
4. Approximate fuel consumption at 2000 m altitude:
- Cruise engine mode: 10.4 l/min
- Combat engine mode: 13.6 l/min
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