Bf 109 F-2 / IL-2 Sturmovik: Great Battles
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Fighter
Bf 109 F-2
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. The result was the Bf 109 F "Friedrich."

The fighter received a new, more aerodynamically advanced engine cowling with an enlarged propeller cowl, improved coolant radiators in underwing mounts, a tail section without external bracing, and a semi-retractable tailwheel assembly. The track width of the main landing gear struts was slightly increased to improve landing characteristics. Special fairings on the wing of the "Emil" for the cannon magazines worsened the aerodynamics, so on the "Friedrich," all weapons were placed in the fuselage. These included a motor cannon, mounted between the cylinder banks and fired through the propeller shaft, and two synchronized 7.92 mm machine guns, similar to those of the previous series.

Originally it was planned to install a new version of the DB 601E engine with a takeoff power of 1350 hp and a new, more advanced Mauser MG 151 cannon, which had a higher rate of fire in comparison to MG/FF cannons, but neither the engine nor the cannon could be completed in time for the start of aircraft production. Pre-production versions of the Bf 109 F-0 and the first production Bf 109 F-1s were equipped with DB 601N engines and a 20 mm MG/FF cannon. As a result, the weight of the secondary salvo was almost halved compared to the previous model, but maneuverability and climb rate were significantly improved.

In September 1940, Mauser specialists succeeded in putting into serial production the MG 151 cannon with a caliber of 15 mm. This weapon with 200 rounds of ammunition was installed on the new production model of the Bf 109 F-2, but pilots continued to complain about the weakness of the armament. Like the previous series, the F-2 was powered by the DB 601N engine, which allowed it to reach speeds of up to 600 km/h at altitude.

Three modifications of the Bf 109 F-2 are known. The first two were produced in small numbers, while the third was a prototype:
  • F-2/B fighter-bomber with ETC 500 bomb rack under the fuselage for bombs up to 250 kg;
  • F-2/Trop tropical fighter with dust filter and new blower air intake;
  • F-2/Z high altitude fighter with nitrous oxide injection system, propeller with widened blades, blower air intake as on F-2/Trop, and large capacity oil cooler.

The total number of F-model Messerschmitts produced before June 22, 1941, can be estimated at around 1,850 units. In terms of flight characteristics, these machines surpassed all the fighters of the Allies in the anti-Hitler coalition, yielding only to some in horizontal maneuverability. Luftwaffe pilots won resounding victories with this variant in North Africa and on the Eastern Front in 1941. It was with this model that Messerschmitt's fame reached its peak, and the Bf 109 F was hailed as the perfect fighter.

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: 151..168 km/h
Indicated stall speed in takeoff/landing configuration: 144 km/h..159 km/h
Dive speed limit: 850 km/h
Maximum load factor: 11 G
Stall angle of attack in flight configuration: 19.7 °
Stall angle of attack in landing configuration: 17 °
 
Maximum true air speed at sea level, engine mode - Emergency: 528 km/h
Maximum true air speed at 2000 m, engine mode - Emergency: 563 km/h
Maximum true air speed at 5000 m, engine mode - Emergency: 606 km/h
 
Service ceiling: 11500 m
Climb rate at sea level: 16.4 m/s
Climb rate at 3000 m: 14.1 m/s
Climb rate at 6000 m: 10 m/s
 
Maximum performance turn at sea level: 23.6 s, at 270 km/h IAS.
Maximum performance turn at 3000 m: 29.0 s, at 270 km/h IAS.
 
Flight endurance at 3000 m: 2.4 h, at 350 km/h IAS.
 
Takeoff speed: 145..175 km/h
Glideslope speed: 185..195 km/h
Landing speed: 135..145 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 Boosted power.
 
Engine:
Model: DB-601N
Maximum power in Boosted mode at 5500 m: 1220 HP
Maximum power in Emergency mode at sea level: 1175 HP
Maximum power in Emergency mode at 4900 m: 1175 HP
Maximum power in Combat mode at sea level: 1015 HP
Maximum power in Combat mode at 4900 m: 1045 HP
 
Engine modes:
Nominal (unlimited time): 2300 RPM, 1.15 ata
Combat power (up to 30 minutes): 2400 RPM, 1.25 ata
Emergency power (up to 3 minutes): 2600 RPM, 1.35 ata
Boosted 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: 110 °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: 2171 kg
Minimum weight (no ammo, 10% fuel): 2445 kg
Standard weight: 2789 kg
Maximum takeoff weight: 3092 kg
Fuel load: 304 kg / 400 l
Useful load: 921 kg
 
Forward-firing armament:
15mm gun "MG 151/15", 200 rounds, 700 rounds per minute, nose-mounted
2 x 7.92mm machine gun "MG 17", 500 rounds, 1200 rounds per minute, synchronized
20mm gun "MG 151/20", 200 rounds, 700 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: March 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 emergency mode for the radiator shutters, which can be used in specific situations. In this mode, the shutters are forced to be fully opened.
- 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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