Bf 109 K-4 / IL-2 Sturmovik: Great Battles
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Fighter
Bf 109 K-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. 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 the second half of the war, the tension in the skies continued to increase, leading to a sharp rise in aircraft losses. In 1944, the Luftwaffe was fighting at the limit of its capabilities and switched to air defense. The aircraft industry was reorganized to increase production of fighter aircraft. To coordinate all activities related to the serial production of fighters, a "Fighter Headquarters" was created in March 1944 at the Ministry of Aviation, which quickly established cooperation between assembly plants and component suppliers, using the harshest repressive and administrative measures.

In an attempt to keep the well-proven fighter on the assembly line, but to reduce the number of its modifications, the "Headquarters" proposed to create a new model of the Bf 109. The aircraft was to receive a new modification of the DB 605 engine — the 605D, which was a unified version with the introduction of all previous modifications in series production (larger supercharger, fuel system allowing to operate on different types of fuel, and use of the MW 50 boost system). This is how the last production version of the Bf 109 K "Kurfürst" was created.

The Messerschmitt designers planned to increase flight performance primarily through improved aerodynamics.

The first pre-production Bf 109 K-0 was built in September 1944. It had an Erla-type canopy, a wooden tail, and a retractable tail wheel on an extended strut, which finally made it possible to reduce the aircraft's landing angle from 14 to 13 degrees and solve the problem of uneven airflow over the wings, thus reducing the number of accidents during landings. Several variants of the new aircraft were developed, but only the Bf 109 K-4, which received the DB 605 DB engine as standard, went into production in the early fall of 1944. This engine could run on B4 fuel with MW50 injection or on C3 fuel without MW 50, which gave a takeoff power of 1850 hp in both cases. At the end of the war, a variant of the DB 605 DS engine was installed on some aircraft, which developed up to 2000 hp on C3 fuel with MW 50 injection and increased turbocharging. Standard armament included a 30 mm MK 108 cannon and two synchronized MG 131 machine guns.

The test reports noted that the Kurfüst differed from the Gustav in the following main features
  • The wing installation was changed;
  • Smoother upper surface of the wing;
  • Improved shape of the cockpit-fuselage interface;
  • New air intakes for supercharging;
  • Improved engine cooling system;
  • More efficient oil coolers were installed;
  • More advanced exhaust systems with a more jet-like effect;
  • Engine cowling with improved aerodynamics.

In tests with production aircraft, the Bf 109 K was about 35-40 km/h faster than the Bf 109 G with the same engines and external mountings.

Field conversion kits for the Bf 109 K-4 included:
  • R1 - mounting of an ETC 500IXb or 503 rack for carriage of one 250 kg or 500 kg bomb;
  • R3 - mounting of a rack for a 300-liter drop tank;
  • R5 - two MG 151/20 cannons in underwing gunpods

The first Kurfüsts rolled off the assembly lines in October 1944 and were delivered to training and air defense units in Germany. During the winter, the number of units that were fully or partially converted to the Bf 109 K increased steadily, with the Kurfürst being delivered primarily to the Western Front. Bf 109 K-4 fighters took part in the last major Luftwaffe operation called "Bodenplatte" - the attack on Allied airfields in Belgium and Holland on January 1, 1945.

According to one of the last programs of the German aircraft industry, the production of Kurfüsts was to exceed 12700 machines in the period from July 1944 to March 1946. The actual number of aircraft built is not known: it is believed that no more than 1200 Bf 109 K-4 were built, of which 534 were delivered by November 30, 1944.

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: 167..190 km/h
Indicated stall speed in takeoff/landing configuration: 160..181 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 °
 
DB-605DB engine:
 
Maximum true air speed at sea level, engine mode - Emergency: 599 km/h
Maximum true air speed at 7500 m, engine mode - Emergency: 702 km/h
Maximum true air speed at sea level, engine mode - Combat: 543 km/h
Maximum true air speed at 8000 m, engine mode - Combat: 684 km/h
 
Service ceiling: 12300 m
Climb rate at sea level: 20.5 m/s
Climb rate at 3000 m: 17.5 m/s
Climb rate at 6000 m: 13.4 m/s
 
Maximum performance turn at sea level: 24.0 s, at 270 km/h IAS.
Maximum performance turn at 3000 m: 32.2 s, at 270 km/h IAS.
 
DB-605DC engine:
 
Maximum true air speed at sea level, engine mode - Emergency: 614 km/h
Maximum true air speed at 6200 m, engine mode - Emergency: 713 km/h
Maximum true air speed at sea level, engine mode - Combat: 536 km/h
Maximum true air speed at 8000 m, engine mode - Combat: 684 km/h
 
Service ceiling: 12300 m
Climb rate at sea level: 19.7 m/s
Climb rate at 3000 m: 17.4 m/s
Climb rate at 6000 m: 13.3 m/s
 
Maximum performance turn at sea level: 24.2 s, at 270 km/h IAS.
Maximum performance turn at 3000 m: 32.3 s, at 270 km/h IAS.
 
Flight endurance at 3000 m: 2.15 h, at 350 km/h IAS.
 
Takeoff speed: 160..190 km/h
Glideslope speed: 200..215 km/h
Landing speed: 155..160 km/h
Landing angle: 12.5 °
 
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-605DB
Maximum power in Emergency mode with MW-50 at sea level: 1850 HP
Maximum power in Emergency mode with MW-50 at 6000 m: 1600 HP
Maximum power in Combat mode at sea level: 1430 HP
Maximum power in Combat mode at 6800 m: 1285 HP
 
Engine modes:
Nominal (unlimited time): 2400 RPM, 1.35 ata
Combat power (up to 30 minutes): 2600 RPM, 1.45 ata
Emergency power (up to 10 minutes): 2800 RPM, 1.8 ata
 
Engine:
Model: DB-605DC
Maximum power in Emergency mode with MW-50 at sea level: 2000 HP
Maximum power in Emergency mode with MW-50 at 4900 m: 1800 HP
Maximum power in Combat mode at sea level: 1370 HP
Maximum power in Combat mode at 6800 m: 1285 HP
 
Engine modes:
Nominal (unlimited time): 2400 RPM, 1.35 ata
Combat power (up to 30 minutes): 2600 RPM, 1.45 ata
Emergency power (up to 10 minutes): 2800 RPM, 1.98 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: 95 °C
 
Supercharger gear shift altitude: fluid coupling 
 
Empty weight: 2754 kg
Minimum weight (no ammo, 10% fuel): 3006 kg
Standard weight: 3361 kg
Maximum takeoff weight: 3891 kg
Fuel load: 304 kg / 400 l
Useful load: 1137 kg
 
Forward-firing armament:
30mm gun "MK 108", 65 rounds, 650 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)
 
Bombs:
249 kg general purpose bomb "SC 250"
500 kg general purpose bomb "SC 500"
 
Length: 8.94 m
Wingspan: 9.97 m
Wing surface: 16.1 m²
 
Combat debut: October 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.
- The aircraft is equipped with MW-50 water-methanol mixture injection system that prevents the engine detonation in the emergency power mode. 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 at the emergency mode without the water-methanol mixture or at altitudes higher than 6 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: 6.6 l/min
- Combat engine mode: 11.1 l/min
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