Bf 109 E-7 / IL-2 Sturmovik: Great Battles
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Fighter
Bf 109 E-7
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 the continuous improvements made based on the experience of use in combat. 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 at the beginning of the Second World War. Emil prototypes started flying in the summer of 1938, and the first production Bf 109 E-1 was delivered to the Luftwaffe in January 1939. The fighter was mass-produced and constantly modernized by various companies from the beginning of the war.

In the early fall of 1940, the Bf 109 E-7 with the DB601N engine and a takeoff power of 1215 hp began to roll off the assembly lines. It differed from the previous modifications in that it could be equipped with a 250 kg bomb or a 300-liter tank suspended from the ETC 500 universal mount under the fuselage. The use of a drop tank increased the range, which was insufficient. Externally, the aircraft of this modification were distinguished by a pointed propeller cowl, and some of them were equipped with armored glass in the front part of the canopy.

The armament of the aircraft remained the same as on the previous modifications and consisted of two synchronized 7.92 mm machine guns in the fuselage and two 20 mm "Oerlikon" MG/FF cannons in the wing. The placement of the cannon magazine in the wing of the Messerschmitt necessitated the installation of convex fairings on the underside of the wing, to the detriment of its aerodynamics.

The Bf 109 E-7/U2 attack variant was characterized by the presence of 5mm armor plates under the oil cooler and fuel pumps to protect it from ground fire.

Specially prepared for operation in hot climates, the Bf 109 E-7/Trop variants were delivered to fighter units fighting in the Mediterranean theater. In addition to a sand filter mounted at the inlet of the engine fan, these aircraft were equipped with a special emergency kit and an attachment for an umbrella to cover the cockpit. After take-off, the pilot would open the flap and the air to the compressor would be bypassed to prevent loss of engine power due to air intake through the filter.

The Bf 109 E-7/Z (80 units produced) was the first to use the GM-1 nitrous oxide injection boost system, which helped increase the fighter's ceiling, speed, and rate of climb at high altitudes. In a report on the tests of a Bf 109 E-7/Z dated December 8, 1940, the following results were stated: in the altitude range from 8000 to 11000 m, the speed of the fighter with the GM-1 system enabled increased by 60-105 km/h, and the rate of climb by 2-3 m/s, which is very significant for high altitudes. Although the GM-1 boost system proved effective and was used in many subsequent modifications of the Bf 109, its use was accompanied by an increase in the aircraft's flight weight and a decrease in its performance at low altitudes, where the system did not provide any performance improvement.

A total of 438 (other reports say 750) Bf 109E-7s were built.

From 1939, the Bf 109 E showed a clear superiority over its main rivals in aerial combat. One ace who started his career with the Bf 109 E was the famous Adolf Galland. The highlight of the Emil's career was its participation in the Battle of Britain. However, its not very successful actions in this operation became one of the reasons for stopping the production of this model. Instead of it a new variant, the Bf 109 F, came into service. The last major operation in which the Luftwaffe's Emils participated was the attack on the USSR, but by 1942 they had practically disappeared from German units on the Eastern Front, remaining in service with the air forces of Spain, Switzerland, Hungary, Bulgaria, and Slovakia.

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: 152..159 km/h
Indicated stall speed in takeoff/landing configuration: 147..146 km/h
Dive speed limit: 850 km/h
Maximum load factor: 11 G
Stall angle of attack in flight configuration: 20 °
Stall angle of attack in landing configuration: 16.6 °
 
Maximum true air speed at sea level, engine mode - Emergency: 477 km/h
Maximum true air speed at 2000 m, engine mode - Emergency: 520 km/h
Maximum true air speed at 5000 m, engine mode - Emergency: 564 km/h
 
Service ceiling: 10500 m
Climb rate at sea level: 14 m/s
Climb rate at 3000 m: 13.3 m/s
Climb rate at 6000 m: 7 m/s
 
Maximum performance turn at sea level: 20.5 s, at 270 km/h IAS.
Maximum performance turn at 3000 m: 25.5 s, at 270 km/h IAS.
 
Flight endurance at 3000 m: 2.2 h, at 350 km/h IAS.
 
Takeoff speed: 140..170 km/h
Glideslope speed: 180..190 km/h
Landing speed: 130..140 km/h
Landing angle: 14.3 °
 
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-601A
Maximum power in Boosted mode at sea level: 1100 HP
Maximum power in Emergency mode at sea level: 990 HP
Maximum power in Emergency mode at 4500 m: 1020 HP
Maximum power in Combat mode at sea level: 910 HP
Maximum power in Combat mode at 5000 m: 960 HP
 
Engine modes:
Nominal (unlimited time): 2200 RPM, 1.15 ata
Combat power (up to 30 minutes): 2300 RPM, 1.23 ata
Emergency power (up to 5 minutes): 2400 RPM, 1.3 ata
Boosted power (up to 1 minute): 2400 RPM, 1.4 ata
 
Water rated temperature in engine output: 94 °C
Water maximum temperature in engine output: 100 °C
Oil rated temperature in engine intake: 30..75 °C
Oil maximum temperature in engine intake: 80 °C
Oil rated temperature in engine output: 95 °C
Oil maximum temperature in engine output: 105 °C
 
Supercharger gear shift altitude: fluid coupling 
 
Empty weight: 2049 kg
Minimum weight (no ammo, 10% fuel): 2340 kg
Standard weight: 2614 kg
Maximum takeoff weight: 2893 kg
Fuel load: 304 kg / 400 l
Useful load: 844 kg
 
Forward-firing armament:
2 x 20mm gun "MG FF", 60 rounds, 540 rounds per minute, wing-mounted
2 x 7.92mm machine gun "MG 17", 1000 rounds, 1200 rounds per minute, synchronized
 
Bombs:
Up to 4 x 55 kg general purpose bombs "SC 50"
249 kg general purpose bomb "SC 250"
 
Length: 8.8 m
Wingspan: 9.9 m
Wing surface: 16.4 m²
 
Combat debut: August 1940
 
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.
- 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.
- Water and oil radiator shutters are controlled manually.
- 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 42°.
- 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 radiator control handle: open
- recommended position of the water radiator control handle: close
- 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
 
3.1 Recommended positions of the oil radiator control handle for various flight modes:
- cruise flight: open 50%
- combat: open 50%
- takeoff: open
 
3.2 Recommended positions of the water radiator control handle for various flight modes:
- cruise flight: open 50%
- combat: open 50%
- takeoff: open 50%
 
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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