Bf 110 G-2 / IL-2 Sturmovik: Great Battles
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Fighter
Bf 110 G-2
History
Specifications

The Bf 110 was designed in 1934 as a long-range multi-role fighter and bomber escort. At the time, this idea was being embraced by almost every country in the world, and creating the latest aircraft seemed like a logical step to take. The prototype first flew on May 12, 1936, and production of the aircraft began in August 1937, but the first production version with Daimler-Benz engines did not begin to be built until 1939 due to a delay in the production of the DB601 engines.

However, despite its good speed characteristics and powerful armament, this aircraft proved to be unsuitable for fighter missions under combat conditions. The Battle of Britain demonstrated the failure of the "heavy fighter" concept. Because of its heavy weight, the Bf 110 was inferior in climb and maneuverability to all the enemy's main single-engine fighters, so it was regarded primarily as a fighter-bomber and its production was curtailed. It was planned to start production of a new model — the Me 210. However, difficulties with its development forced the resumption of serial production of the Bf 110 in 1942. This naturally led to the decision to create an improved modification of this aircraft — thus the Bf 110 G was born.

The first modification of the Bf 110 G-2 fighter-bomber, which could be used as a "heavy fighter," went into production in May 1942.

The Bf 110 G-2 was a two-seat, twin-engined, all-metal low-wing aircraft powered by the DB 605B-1. It had retractable landing gear and no external struts. The DB 605B-1 developed 1,475 hp at takeoff and 1,355 hp at an altitude of 5,700 meters in emergency mode. In addition, due to the increased weight of the aircraft and armament, reinforced landing gear struts were installed and some minor improvements in design and equipment were introduced.

The offensive armament consisted of two 7.92 mm MG 17 machine guns and two 20 mm MG 151/20 cannons. The defensive armament was also strengthened by replacing the 7.92 mm MG 15 turret machine gun with a twin MG 81Z of the same caliber. Under the fuselage were two ETC 500 racks, which could be replaced by two 20 mm MG 151/20 cannons (200 rounds each, such a modification was called Rüstsatz/R M1).

The mounts for the two 300-liter drop tanks under the wings could be replaced by four ETC 50/VIII racks to increase the bomb load from 1,000 to 1,200 kg.

The following field conversion kits were available for the Bf 110 G-2:
  • G-2/R1: with 37 mm BK 3.7 (Flak 18) cannon under the fuselage instead of the MG 151/20 cannons. Ammunition was 72 rounds in 6-round magazines located in the fuselage near the gunner's position, who loaded the gun manually;
  • G-2/R2: with GM1 boost system. A 440 kg nitrous oxide tank was installed in place of the gunner, and the rear cockpit armor and MG 81Z machine guns were removed;
  • G-2/R3: instead of four MG 17 nose machine guns, two 30 mm MK 108 cannons (135 rounds each) were installed.
  • G-2/R4: simultaneously modified R1 and R3;
  • G-2/R5: retrofitted with R1, R2, and R3 types at the same time.

A total of 797 aircraft of this modification were built. On the Eastern Front, the Bf 110 was mainly used for attacks on ground targets and as a reconnaissance aircraft, but for some time it was also used as a night fighter, e.g. in 10.(Nachtjagd)/ZG 1 (Taman, Bagerovo airfield).

An attempt was made to use the Bf 110 G-2/R1 as an anti-tank aircraft, but this idea was quickly abandoned due to its high vulnerability and the difficulty of operating from primitive airfields, and it was transferred to the Reich Air Defense. The 37 mm cannon proved effective against bombers: a single hit usually destroyed a B-17 heavy bomber. On the other hand, the weight of the cannon and the additional drag of the fairing made the Bf 110 extremely vulnerable to fighter escorts. In the summer of 1943, almost all surviving Bf 110s were recalled from the Eastern Front to German air defense units.

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

2. "Wings of the Luftwaffe" Translation of W. Green's book "Warplanes of the Third Reich" by A. Firsov, 1993.

3. A. Larionov, R. Maraev "Goering's destroyer" Journal "Aviation and Time", № 5, 2010

4. Materials from the site airwar.ru

Indicated stall speed in flight configuration: 160..190 km/h
Indicated stall speed in takeoff/landing configuration: 141..168 km/h
Dive speed limit: 740 km/h
Maximum load factor: 11 G
Stall angle of attack in flight configuration: 20.3 °
Stall angle of attack in landing configuration: 17.4 °
 
Maximum true air speed at sea level, engine mode - Combat: 489 km/h
Maximum true air speed at 2000 m, engine mode - Combat: 533 km/h
Maximum true air speed at 6500 m, engine mode - Combat: 581 km/h
 
Service ceiling: 10800 m
Climb rate at sea level: 15.6 m/s
Climb rate at 3000 m: 14.1 m/s
Climb rate at 6000 m: 10.7 m/s
 
Maximum performance turn at sea level: 23.5 s, at 270 km/h IAS.
Maximum performance turn at 3000 m: 31.2 s, at 270 km/h IAS.
 
Flight endurance at 3000 m: 4.0 h, at 300 km/h IAS.
 
Takeoff speed: 190..230 km/h
Glideslope speed: 210..230 km/h
Landing speed: 150..170 km/h
Landing angle: 10.7 °
 
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 Combat power, turn times are given for Emergency power.
 
Engine:
Model: DB-605B
Maximum power in Emergency mode at sea level: 1480 HP
Maximum power in Emergency mode at 5600 m: 1360 HP
Maximum power in Combat mode at sea level: 1310 HP
Maximum power in Combat mode at 5800 m: 1250 HP
 
Engine modes:
Nominal (unlimited time): 2300 RPM, 1.15 ata
Combat power (up to 30 minutes): 2600 RPM, 1.3 ata
Emergency power (up to 1 minute): 2800 RPM, 1.42 ata
 
Water rated temperature in engine output: 100..102 °C
Water maximum temperature in engine output: 115 °C
Oil rated temperature in engine intake: 70..80 °C
Oil maximum temperature in engine intake: 85 °C
 
Supercharger gear shift altitude: fluid coupling 
 
Empty weight: 5905 kg
Minimum weight (no ammo, 10% fuel): 6335 kg
Standart weight: 7514 kg
Maximum takeoff weight: 8928 kg
Fuel load: 1003 kg / 1270 l
Useful load: 3023 kg
 
Forward-firing armament:
4 x 7.92mm machine gun "MG 17", 1000 rounds, 1200 rounds per minute, nose-mounted
20mm gun "MG 151/20", 400 rounds, 700 rounds per minute, nose-mounted left
20mm gun "MG 151/20", 350 rounds, 700 rounds per minute, nose-mounted right
2 х 20mm gun "MG 151/20", 200 rounds, 700 rounds per minute, nose-mounted (modification)
37mm gun "BK3.7", 66 rounds, 160 rounds per minute, nose-mounted (modification)
 
Defensive armament:
Backward: 2 x 7.92mm machine guns "MG 81", 750 rounds, 1600 rounds per minute
 
Bombs:
Up to 12 x 55 kg general purpose bombs "SC 50"
Up to 2 x 249 kg general purpose bombs "SC 250"
Up to 2 x 500 kg general purpose bombs "SC 500"
1090 kg general purpose bomb "SC 1000"
 
Length: 12.1 m
Wingspan: 16.3 m
Wing surface: 38.4 m²
 
Combat debut: Autumn 1942
 
Operation features:
- The aircraft has a wide automatization of the engine systems, in fact, to control speed it is only necessary to use the throttle lever. There is no need to manually set engine revolutions and mixture or supercharger gear in normal flight.
- Water and oil radiator shutters are controlled manually. The oil radiator control has five fixed positions. The water radiator control has nine fixed positions.
- The aircraft has a fuel gauge which shows remaining fuel in fuel tanks depending on switch position. In game the fuel indicator switch changes by pressing (RShift+I).
- Propellers have a feathering system which should be activated in case of engine damage to reduce drag of the propeller in auto-rotation.
- To reduce swinging during taxiing due to prop-wash it is necessary to use asymmetrical engines thrust. It is recommended to give the left engine 20% more power. Also, the prop pitch control should be switched to manual mode and pitch should be reduced to minimum.
- The aircraft has only pitch and yaw flight-control trimmers.
- The aircraft has automatic wing slats. They deploy when the high angle of attack increases which makes pre-stall softer.
- Landing flaps have a hydraulic actuator and they can be extended to any angle up to 50°.
- The aircraft has an automatically controlled horizontal stabilizer. An automatic control system adjusts the stabilizer angle depending on the extended angle of the landing flaps.
- 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 a fuel gauge which shows the remaining fuel in one of four fuel tanks depending on the switch position. Also, the airplane has a low fuel warning light (50 liters) for each tank.
- The design of the cockpit canopy does not allow it to be opened during flight. The canopy should be closed before takeoff to prevent damage. The canopy has an emergency release system for bailouts.
- The aircraft is equipped with an automatic bomb salvo controller, it allows you to choose which bomb-racks to be released (central belly, left and right wing) and to switch the bomb salvo (single release or release all bombs).
- Reloading of BK37 gun is performed by the rear gunner at the pilot`s command.
- The gunsight has a sliding sun-filter.
 
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: auto prop pitch control
- recommended position of the throttle lever: 15%
 
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 75%
 
3.2 Recommended positions of the water 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 75%
 
4. Approximate fuel consumption at 2000 m altitude:
- Cruise engine mode: 11.2 l/min
- Combat engine mode: 13.8 l/min
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