Bf 109 G-6 / IL-2 Sturmovik: Great Battles
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Fighter
Bf 109 G-6
History
Specifications

The Messerschmitt Bf 109, the most mass-produced fighter of Hitler's Germany, appeared in 1934 in response to the Luftwaffe's request for the latest single-engine monoplane fighter. The prototype's first flight took place on May 28, 1935, and from 1936 to 1942, 6 models were built — from the Bf 109 A "Anton" to the Bf 109 G "Gustav."

In all military campaigns since 1938, the Bf 109 demonstrated clear air superiority over its main rivals — even the relative failure in the Battle of Britain did not shake the Luftwaffe leadership's confidence in the aircraft's capabilities. But in the conditions of rapidly increasing numerical superiority of the Allied fighters, it became simply impossible to shoot down heavy bombers and armored Il-2s with rifle-caliber weapons. Attempts to increase the fighter's firepower by installing cannons in gunpods were unsuccessful. The result was a loss of maneuverability, and it was difficult to engage enemy fighters. The idea of increasing the fighter's firepower by replacing the 7.92 mm machine guns with large-caliber ones was born after numerous complaints from pilots. The installation of MG 131 machine guns with sufficient ammunition required changes in the design of the engine cowls with the addition of characteristic bulges on the sides, which were called "bumps" — this eventually became the nickname of the entire aircraft.

This fighter was available in a conventional version as well as a tropical version without a pressurized cabin and with the DB-605A-1 engine. The Bf 109 G-6 had many variants during series production, especially in terms of armament and engine boost systems.

The following production variants were built:
  • U2 - built-in GM-1 high-altitude boost system;
  • U3 - built-in, non-removable MW 50 boost system kit for increasing flight speed at low and medium altitudes by injecting a water-methanol-oil mixture. From May 1944 this installation became standard and was installed in all fighters not equipped with GM-1;
  • U4 - installation of 30 mm MK 108 cannon between the engine cylinder banks, firing through the propeller shaft;
  • U5 - the same installation as U4, plus two more MK 108 cannons in gunpods (unlike the pre-production variant, the cannons were mounted on the underside of the wings and could not be removed). This kit was planned but never used.
  • U6 - MK 103 30mm cannon mounted between the engine cylinder banks. This kit was planned but was never used.

It should be noted that the MK 103 and the MK 108 had different ammunition for the same caliber, but the MK 108 had a higher rate of fire and lower recoil with less powerful ammunition, making it best suited for use on fighters in aerial combat.

In October 1943, the Bf 109 G-6/U4/R4 was built and tested with an unusually powerful armament consisting of three MK 108 30mm cannons (total of 165 rounds) and two 13mm machine guns. It was found that the guns were not yet fully developed, with frequent stoppages in firing.

Field conversion kits for the G-6 offered a variety of options:
  • R1 - Removable ETC 500/IX bomb rack under the fuselage to carry an SC 250 bomb;
  • R2 - Installation of an RB 50/30 camera behind the cockpit and installation of an ETC 50 VIId pylon for four 50 kg bombs;
  • R3 - Special rack for 300-liter drop tank only;
  • R4 - SD-2 fragmentation bomb container carrier mounted under the fuselage;
  • R6 - similarly suspended gunpods, but with 20 mm MG 151/20 cannons;
  • R7 - installation of radio direction-finding equipment;
  • R8 - photographic camera gun in the leading edge of the starboard wing.

The Bf 109 G-6, which was in production from February 1943 to the summer of 1944, was the longest-lived member of the Bf 109 family and its most mass-produced variant: more than 12,200 aircraft of all variants were built. It was believed that the fighter could be used in different climatic conditions from the Arctic Circle to Africa, and could fight effectively both close to the ground, as was often the case on the Soviet-German front, and at high altitude against groups of Allied heavy bombers.

Sources used:

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

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

3. "Yak-1,7,9,3/ Bf 109 fighters" Journal of Aviation and Cosmonautics, 5-6, 1999.

4. Materials of the site airwar.ru

Indicated stall speed in flight configuration: 160..177 km/h
Indicated stall speed in takeoff/landing configuration: 153..169 km/h
Dive speed limit: 850 km/h
Maximum load factor: 10.5 G
Stall angle of attack in flight configuration: 19.8 °
Stall angle of attack in landing configuration: 17 °
 
Maximum true air speed at sea level, engine mode - Emergency: 529 km/h
Maximum true air speed at sea level, engine mode - Combat: 505 km/h
Maximum true air speed at 2000 m, engine mode - Combat: 547 km/h
Maximum true air speed at 7000 m, engine mode - Combat: 632 km/h
 
Service ceiling: 11800 m
Climb rate at sea level: 20.1 m/s
Climb rate at 3000 m: 18.8 m/s
Climb rate at 6000 m: 15.2 m/s
 
Maximum performance turn at sea level: 21.5 s, at 270 km/h IAS.
Maximum performance turn at 3000 m: 28.0 s, at 270 km/h IAS.
 
Flight endurance at 3000 m: 2.2 h, at 350 km/h IAS.
 
Takeoff speed: 155..180 km/h
Glideslope speed: 195..205 km/h
Landing speed: 150..155 km/h
Landing angle: 13.7 °
 
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 and turn times are given for Combat power.
 
Engine:
Model: DB-605A
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: 2583 kg
Minimum weight (no ammo, 10% fuel): 2734 kg
Standard weight: 3100 kg
Maximum takeoff weight: 3400 kg
Fuel load: 304 kg / 400 l
Useful load: 817 kg
 
Forward-firing armament:
20mm gun "MG 151/20", 200 rounds, 700 rounds per minute, nose-mounted
2 x 13mm machine gun "MG 131", 300 rounds, 900 rounds per minute, synchronized
2 x 20mm gun "MG 151/20", 135 rounds, 700 rounds per minute, wing-mounted (modification)
30mm gun "MK 108", 65 rounds, 650 rounds per minute, nose-mounted (modification)
 
Bombs:
Up to 4 x 55 kg general purpose bombs "SC 50"
249 kg general purpose bomb "SC 250"
 
Length: 8.94 m
Wingspan: 9.97 m
Wing surface: 16.1 m²
 
Combat debut: february 1943
 
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.
- In addition to full-automatic mode there is a special manual control mode for the radiator shutters, which can be used in specific situations.
- To reduce swinging during taxiing due to prop-wash the prop pitch control should be switched to manual mode and pitch should be reduced to minimum.
- The aircraft has no flight-control trimmers. Airplane is equipped with bendable trim tabs that can be set pre-flight by ground personnel.
- The aircraft has a manually controlled horizontal stabilizer. It should be set to +1° before takeoff and to -4°...-5° before landing. Also, it may be used to trim the flight stick during the flight. In a deep dive the stabilizer should be set so that the pilot must push the flight stick forward to maintain the dive angle.
- The aircraft has automatic wing slats. They deploy when the high angle of attack increases which makes pre-stall softer.
- The aircraft has a manual mechanical system for retracting the landing flaps, for this reason it is necessary to extend landing flaps well before final approach. Markers on the left-wing flap indicate how far the flaps are extended. The flaps can be extended to any angle up to 40°.
- The aircraft has a manual tailwheel lock. Wheel should be locked when taxiing straight for a long distance and before 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 total fuel remaining. Also, it has an emergency fuel warning light (80 liters).
- 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 control system for the bomb rack only allows to drop bombs one by one.
- 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/water radiator control handle: auto radiators control
- recommended position of the prop pitch control handle: auto prop pitch control
- recommended position of the throttle lever: 10%
- before taxiing, you must unlock the tailwheel
 
2. Recommended mixture control lever positions for various flight modes: auto mixture control
 
3. Recommended positions of the radiators control handle for various flight modes: auto radiators control
 
4. Approximate fuel consumption at 2000 m altitude:
- Cruise engine mode: 5.2 l/min
- Combat engine mode: 8.6 l/min
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