He 111 H-6 / IL-2 Sturmovik: Great Battles
Close
menu
Bomber
He 111 H-6
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.

A mass modification produced from April 1941 was the He 111 H-6. It had Jumo 211F-1 engines combined with wide-blade propellers and single exhaust pipes instead of manifolds. Late production aircraft were equipped with Jumo 211F-2 engines.

The plane's wing was a two-spar with a stressed skin, typical of aircraft with semi-elliptical sections, with a straight leading edge installed with a slight sweep. The center section was integral to the all-metal fuselage, which had three main frames and several auxiliary frames connected by a large number of spars and stringers. The slotted flaps were operated by the pilot. The main landing gear was double and hydraulically retracted into the nacelles.

The He 111 H-6 was characterized by an improved defensive armament, already introduced with the H-2 modification. Initially, MG 17 machine guns were installed in the nose and in the front of the underbelly gondola, but in different variations (in one or both positions). Later the machine gun could be replaced by an MG/FF cannon. Some planes had a 7.92 mm MG 17 machine gun in the tail cone, while others had an aircraft grenade launcher in the same position, from which grenades were thrown with parachutes. Both the additional machine gun and the grenade launcher ensured the destruction of the area behind the tail, close to the upper firing point. However, the effectiveness of these systems was low.

The He 111 H-6 was equipped with both internal and external suspension points and could carry up to 2500 kg of bombs or aircraft mines and torpedoes. As a torpedo bomber, the H-6 carried a pair of 765 kg LTF 5b torpedoes on PVC mounts.

In 1942, German designers attempted to equip the mass-produced He 111 H-6 with new types of weapons: increasingly sophisticated means of aerial warfare were being developed in Germany. One of these was the FX 1400 "Fritz X" radio-controlled bomb. In the spring of 1942, several H-6s equipped with FuG 203 control system transmitters were used to test this bomb in northern Italy. Despite some successes, the H-6 proved to be unsuitable for employing such weapons under combat conditions. Other H-6s were used for test drops of BV 246 gliding bombs and L10 Friedensengel gliding torpedoes, but all these exotic weapons were only tested on the H-6 — it was never used in combat.

The aircraft was used as a day and night bomber, minesweeper, torpedo bomber, and sometimes as a transport aircraft. The He 111 H-6 quickly became the most common and widely used Heinkel bomber model: pilots loved it for its ease of control even at maximum load, excellent stability and maneuverability, and technical staff noted its ease of maintenance. Although it was planned that it would be replaced in production by new models, failures in their testing forced the continuation of production of a well-developed machine that required minimal labor costs. The H-6 did not fully meet the requirements of the war on the Eastern Front, so it was built until September 1942, with a total production of 1, 775 planes.

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..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-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, 1.42 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 m²
 
Combat debut: June 1941
 
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, there is dedicated fuel gauge for the fuselage fuel tank. 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: 9.8 l/min
- Combat engine mode: 13.3 l/min
Up