Bf 109 F-4 / IL-2 Sturmovik: Great Battles
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Fighter
Bf 109 F-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.

The Second World War, which began in September 1939, made it necessary to take into account not only operational experience but also accumulated combat experience. Thus, in 1940, the designers began to radically improve the aerodynamics of the fighter to maximize the possibilities of the DB 601 engine. This is how the Bf 109 F "Friedrich" came into being.

In the summer of 1941, Daimler-Benz solved the most serious problems associated with the production of a new variant of the DB 601E engine. Unlike the DB 601N, the engine did not have an automatic boost, which limited the time of operation in this mode to 1 minute. It should be noted that according to the results of tests carried out in the Soviet TsIAM institute, the DB 601E engine developed 1450 hp at an altitude of 2000 m and 1350 hp at an altitude of 5100 m in combat emergency mode, i.e., it significantly exceeded the Soviet M-105PF2 engine.

Messerschmitt planned the next version of the Friedrich as a fighter variant with this engine and the unsuccessful MG/FF motor cannon. Meanwhile, Mauser was finally able to start serial production of a 20 mm version of the MG 151 cannon with a more powerful projectile than the 15 mm cannon installed on the Bf 109 F-2, so it was decided to arm the new aircraft with the MG 151 cannon only. The F-3 version was equipped with a 15 mm cannon, while the Bf 109 F-4 was equipped with a 20 mm cannon. It soon became clear that the latter variant was much more popular with pilots, and the Bf 109 F-4 became the main production version of the aircraft.

The maximum speed at all altitudes was increased by 10-25 km/h compared to the Bf 109 F-2 due to the more powerful engine. The climb rate was also increased. The designers improved the fuel tank protection and the head protection of the pilot.

The armament of the Bf 109 F-4 was controversial among the most experienced German fighter pilots. While Werner Mölders was fully satisfied with the light armament of one 20 mm cannon and two machine guns, Adolf Galland considered the reduction of the aircraft's armament a step backward. As a result of the disputes over armament, Messerschmitt developed a so-called "field retrofit kit" for the Bf 109 F-4, which consisted of a pair of MG 151/20 cannons in underwing pods with 120 rounds per gun. The gunpod-equipped fighter was designated the Bf 109 F-4/R1. The additional armament increased the aircraft's firepower and combat capabilities as a fighter or interceptor but compromised the aircraft's stability and controllability due to increased drag and weight. The aircraft tended to wobble and reduced its ability to engage enemy fighters in dogfights, so fighters without the additional armament were mainly used in combat units.

Sources used:

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

2. "Wings of the Luftwaffe" Translation of W. Creen'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: 154..171 km/h
Indicated stall speed in takeoff/landing configuration: 148..161 km/h
Dive speed limit: 850 km/h
Maximum load factor: 11 G
Stall angle of attack in flight configuration: 19.9 °
Stall angle of attack in landing configuration: 17 °
 
Maximum true air speed at sea level, engine mode - Combat: 522 km/h
Maximum true air speed at 2000 m, engine mode - Combat: 570 km/h
Maximum true air speed at 6000 m, engine mode - Combat: 635 km/h
 
Service ceiling: 11600 m
Climb rate at sea level: 19.5 m/s
Climb rate at 3000 m: 18.8 m/s
Climb rate at 6000 m: 14.9 m/s
 
Maximum performance turn at sea level: 20.3 s, at 270 km/h IAS.
Maximum performance turn at 3000 m: 26.1 s, at 270 km/h IAS.
 
Flight endurance at 3000 m: 2.6 h, at 350 km/h IAS.
 
Takeoff speed: 150..180 km/h
Glideslope speed: 190..200 km/h
Landing speed: 145..155 km/h
Landing angle: 14.8 °
 
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-601E
Maximum power in Emergency mode at sea level: 1350 HP
Maximum power in Emergency mode at 4800 m: 1320 HP
Maximum power in Combat mode at sea level: 1200 HP
Maximum power in Combat mode at 4900 m: 1200 HP
 
Engine modes:
Nominal (unlimited time): 2300 RPM, 1.15 ata
Combat power (up to 30 minutes): 2500 RPM, 1.3 ata
Emergency power (up to 1 minute): 2700 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: 2382 kg
Minimum weight (no ammo, 10% fuel): 2545 kg
Standard weight: 2890 kg
Maximum takeoff weight: 3189 kg
Fuel load: 304 kg / 400 l
Useful load: 807 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 15mm gun "MG 151/15", 135 rounds, 700 rounds per minute, wing-mounted (modification)
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: June 1941
 
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: 6.6 l/min
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