Bf 109 G-6AS / IL-2 Sturmovik: Great Battles
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Fighter
Bf 109 G-6AS
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."

One of the problems faced by the Luftwaffe's fighter units was the different nature of the fighting on the eastern and western fronts. While in the East the fighting took place at low and medium altitudes, in the West the main enemy was high-altitude heavy bombers and escort fighters. To combat them, high-altitude fighter variants and engines were developed. Thus the DB 605AS engine was developed, with a supercharger from the DB 603 engine to increase its altitude. This variant ran on 87-octane B4 fuel. Later, some aircraft were equipped with the DB 605ASM engine with the ability to run on C3 fuel (96 octane) and the installation of the MW 50 boost system. This increased the power to 1800 hp.

It was planned to install more powerful engines, such as the DB 605ASB — it could use B4 fuel with the MW 50 boost system or C3 fuel without it and developed power up to 1850 hp. Also planned was the DB 605ASC engine, which used C3 gasoline with the MW 50 boost system and developed power up to 2000 hp, but reliable data on the use of ASB and ASC engines have not been preserved.

The increased diameter of the supercharger required designing a new, much more spacious cowling. The bulges on the cowl were longer and smoother and covered the supercharger as well as the breech blocks of the machine guns. The left and right sides of the cowl were of different lengths. In addition to the cowl, the aircraft was fitted with a new tail section with a taller tail and an improved "Erla" type cockpit canopy with a significantly reduced number of metal parts on the frame, which improved rearward visibility. This canopy was usually combined with the so-called "Galland armor," which was the replacement of the armor plate (which protected the pilot’s head) with armored glass.

The first Bf 109 G-6/ASs were assigned to the combat units III./JG 1, I./JG 5, and II./JG 11 at the beginning of April 1944. In May, I./JG 3 began to receive these fighters. In June, II./JG 27 received its first Bf 109 G-6/ASs (out of a total of 152 aircraft, including 92 new or converted G-6s). In July 1944 several Bf 109 G-6/ASs were assigned to 1./NJGr 10, and a small number were transferred from I./JG1 to III./JG300. A total of 686 Bf 109 G-6/ASs were built, but only 226 of them were produced in series at the Regensburg factory. The rest were converted from conventional Bf 109 G-6s at Erla, Mimetal, and Blohm und Voss.

At low altitudes, an aircraft without the MW 50 system was practically equal to or slightly worse than conventional Gustavs, but with the boost system, it was superior. At high altitudes, due to the installation of a new supercharger, all characteristics were better than any other Messerschmitt.

Indicated stall speed in flight configuration: 163..180 km/h
Indicated stall speed in takeoff/landing configuration: 151..163 km/h
Dive speed limit: 850 km/h
Maximum load factor: 10.5 G
Stall angle of attack in flight configuration: 19.7 °
Stall angle of attack in landing configuration: 17.2 °
 
DB-605AS engine:
 
Maximum true air speed at sea level, engine mode - Emergency: 523 km/h
Maximum true air speed at 3500 m, engine mode - Emergency: 600 km/h
Maximum true air speed at 9500 m, engine mode - Emergency: 670 km/h
Maximum true air speed at sea level, engine mode - Combat: 505 km/h
Maximum true air speed at 2900 m, engine mode - Combat: 565 km/h
Maximum true air speed at 9000 m, engine mode - Combat: 650 km/h
 
DB-605ASM engine:
 
Maximum true air speed at sea level, engine mode - Emergency: 570 km/h
Maximum true air speed at 2000 m, engine mode - Emergency: 610 km/h
Maximum true air speed at 8000 m, engine mode - Emergency: 690 km/h
Maximum true air speed at sea level, engine mode - Combat: 505 km/h
Maximum true air speed at 2900 m, engine mode - Combat: 565 km/h
Maximum true air speed at 9000 m, engine mode - Combat: 650 km/h
 
Service ceiling: 12100 m
Climb rate at sea level: 17.3 m/s
Climb rate at 3000 m: 16.2 m/s
Climb rate at 6000 m: 12.1 m/s
 
Maximum performance turn at sea level: 23.0 s, at 270 km/h IAS.
Maximum performance turn at 3000 m: 28.5 s, at 270 km/h IAS.
 
Flight endurance at 3000 m: 2.3 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-605AS
Maximum power in Emergency mode at sea level: 1435 HP
Maximum power in Emergency mode at 8000 m: 1200 HP
Maximum power in Combat mode at sea level: 1275 HP
Maximum power in Combat mode at 7800 m: 1150 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
 
Engine:
Model: DB-605ASM
Maximum power in Emergency mode at sea level: 1800 HP
Maximum power in Emergency mode at 6400 m: 1500 HP
Maximum power in Combat mode at sea level: 1250 HP
Maximum power in Combat mode at 7800 m: 1150 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 3 minute): 2800 RPM, 1.7 ata
Emergency power (up to 10 minute with MW-50): 2800 RPM, 1.7 ata (modification)
 
Water rated temperature in engine output: 100..102 °C
Water maximum temperature in engine output: 115 °C
Oil rated temperature in engine intake: 75..80 °C
Oil maximum temperature in engine intake: 85 °C
 
Supercharger gear shift altitude: fluid coupling 
 
Empty weight: 2540 kg
Minimum weight (no ammo, 10% fuel): 2855 kg
Standard weight: 3222 kg
Maximum takeoff weight: 3585 kg
Fuel load: 304 kg / 400 l
Useful load: 1045 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:
249 kg general purpose bomb "SC 250"
 
Rockets:
Two WGr.21 rockets in jettisonable launchers
 
Length: 8.94 m
Wingspan: 9.92 m
Wing surface: 16.2 m²
 
Combat debut: spring 1944
 
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.
- MW-50 water-methanol mixture injection system that prevents the engine detonation in the emergency power mode (modification). It engages automatically when the throttle is set to maximum, there is enough mixture for 25-30 minutes. However, the engine can work up to 10 minutes at this mode, wait for another 10 minutes at the combat mode before engaging the emergency mode again. Attention: running the engine with the water-methanol mixture at altitudes higher than 8 km is forbidden! A pilot can check the system using the injection pressure indicator on the left: its normal pressure is 0.6...0.7 atm, stop using it if the pressure is lower than 0.4 atm and switch the engine to combat mode.
- 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 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: 5.3 l/min
- Combat engine mode: 8.2 l/min
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