Bf 109 G-4 / IL-2 Sturmovik: Great Battles
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Fighter
Bf 109 G-4
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. It was an all-metal low-wing aircraft with a water-cooled engine, retractable landing gear, and a tail wheel. The prototype's first flight took place on May 28, 1935, and in November 1936, the first aircraft were sent for military testing in Spain, where a civil war was raging. This decision was due to the failure of the He 51 biplanes, which were losing air battles to Soviet fighters. The Spanish debut ended successfully for the plane, mainly due to continuous improvements. From 1936 to 1938, 5 models were built — from the Bf 109 A "Anton" to the Bf 109 E "Emil" — and this latter model became the main machine in service with fighter squadrons.

Taking into account the experience of the war, the Bf 109 F "Friedrich" was introduced in 1940, and in early 1942 a new DB 605A engine with a takeoff power of 1457 hp was ready for series production. The increase in power meant an increase in engine weight, which necessitated the strengthening of some structural elements and led to the creation of a new, faster modification known as the Bf 109 G "Gustav." The Bf 109 G-1 and Bf 109 G-2 were followed by the Bf 109 G-3, which was produced in small numbers, and the Bf 109 G-4 with the new DB 605A-1 series engine. In the early period of this engine's use, the so-called "emergency" mode (increased boost of 1.42 ATA to increase performance) was forbidden and the boost was limited to 1.3 ATA due to failures and resulting accidents, but this mode was reintroduced when the causes of the problems were investigated.

Structurally, the B 109 G-4 did not differ much from its predecessor, the G-2, and was also produced with a conventional rather than a pressurized cockpit and without a high-altitude engine boost system. But all aircraft of the G-4 modification (as well as the G-3) had a small but important change in the landing gear design. On all Messerschmitts, the landing gear struts, which were attached to the fuselage, were retracted outward into the wing to increase the width between the wheels. As a result, the load on one side of the wheel was greater than on the other. As a result, with increasing weight on the "Gustavs," even enlarged wheels wore out faster and often broke during landings and taxiing. To eliminate this disadvantage, the wheel rotation axes were rotated almost parallel to the ground. First introduced on the last G-2 series, this design became standard on the G-4. In addition to the landing gear, the radio was replaced with a newer and better model. The aircraft was available in conventional and tropical versions — with dust filters, dust and sand seals, and desert survival kits. In terms of flight and tactical characteristics, it did not differ from the Bf 109 G-2.

The field upgrade kits for the G-2 and G-4 variants differed slightly and were used in much the same way, except that the R6 kit was used much less frequently..
 
  • R1 - installed an ETC 500 rack that could carry a 250 kg bomb or a 300-liter drop tank under the fuselage;
  • R2 - reconnaissance aircraft. The Bf 109 G-4/R2 was transformed into a fighter-bomber reconnaissance plane with an Rb50/30 camera and the ETC 50/VIIId bomb rack designed to carry four SC 50 bombs or a 300-liter drop tank, while similar reconnaissance planes were also produced in factories: such a model was designated Bf 109 G-4/U3.
  • R3 - long-range reconnaissance plane. Under the wing of such a machine were installed racks for carrying two additional drop tanks of 300 liters, which were released in flight when empty of fuel. Instead of an ammunition box, an additional oil tank was installed in front of the cockpit. Fuel was pumped from the outboard tanks to the fuselage tank by the pressure drop caused by the engine’s supercharger. According to some reports, the range of such a reconnaissance plane was 1250 km;
  • R6 - installed two underwing gunpods with 20 mm MG 151/20 cannons;
  • R7 - produced only for the G-4. These aircraft were also equipped with radio direction-finding equipment

The aircraft was built by the same factories as the Bf 109 G of previous modifications. A total of 1242 Bf 109 G-4s were produced between September 1942 and May 1943, including 377 of the tropical variant for use in the Mediterranean.

Bf 109 G-4s were used on all fronts and were delivered to combat units from November 1942.

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: 165..175 km/h
Indicated stall speed in takeoff/landing configuration: 154..167 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: 540 km/h
Maximum true air speed at sea level, engine mode - Combat: 517 km/h
Maximum true air speed at 2000 m, engine mode - Combat: 564 km/h
Maximum true air speed at 7000 m, engine mode - Combat: 640 km/h
 
Service ceiling: 11800 m
Climb rate at sea level: 20.1 m/s
Climb rate at 3000 m: 18.9 m/s
Climb rate at 6000 m: 15.4 m/s
 
Maximum performance turn at sea level: 21.2 s, at 270 km/h IAS.
Maximum performance turn at 3000 m: 27.2 s, at 270 km/h IAS.
 
Flight endurance at 3000 m: 2.4 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: 2506 kg
Minimum weight (no ammo, 10% fuel): 2669 kg
Standard weight: 3014 kg
Maximum takeoff weight: 3303 kg
Fuel load: 304 kg / 400 l
Useful load: 797 kg
 
Forward-firing armament:
20mm gun "MG 151/20", 200 rounds, 700 rounds per minute, nose-mounted
2 x 7.92mm machine gun "MG 17", 500 rounds, 1200 rounds per minute, synchronized
2 x 20mm gun "MG 151/20", 135 rounds, 700 rounds per minute, wing-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: November 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.
- 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: 8.3 l/min
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