Fw 190 A-3 / IL-2 Sturmovik: Great Battles
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Fighter
Fw 190 A-3
History
Specifications

In 1938, the Luftwaffe Technical Directorate, disappointed by the debut of the first Bf 109 series in Spain, asked Focke-Wulf to design a new fighter. A distinctive feature of the new aircraft, whose prototype took to the skies on June 1, 1939, was the use of an air-cooled BMW 139 engine and a hollow prop spinner. Another novelty was the use of a large convex cockpit canopy with a minimum of metal binding parts. The aircraft was characterized by good controllability and low stick loading. However, BMW did not succeed in modifying the 139 engine; instead, the BMW 801 engine was introduced, with a similar diameter, but with more weight and slightly more power. The design of the fighter was modified to accommodate the installation of this engine, and from the fall of 1940 to 1942, aircraft of the A-0, A-1, and A-2 series were delivered to combat units.

In the spring of 1942, the BMW 801D-2 went into series production with a takeoff power of 1700 hp, which differed from previous models by an increased compression ratio in the cylinders and some other improvements. At nominal operation at ground level, the engine developed a power of 1570 hp, and at an altitude of 5200 m - 1420 hp.

The installation of this engine on the plane led to the appearance of the production model Fw 190 A-3, which differed from the A-2 version in the shape of the fairings of the supercharger intake manifolds: if previously the convexity of the nozzle was symmetrical concerning the longitudinal axis, now its upper surface became straight and the rear part of the fairing was raised. Initially, the air from the engine compartment passed through simple slots, and after the appearance of controlled flaps on the A-4 model, which made it possible to modify the volume of air passing through, aircraft began to be modified by installing these same flaps.

The armament of the A-3 consisted of four cannons and two machine guns: two MG 151/20 cannons in the wing roots, two MG/FF cannons in the outer wing sections, and two synchronized MG 17 machine guns in the forward fuselage.

The following modifications were made:
  • A-3/U1: only one built with extended forward fuselage, the prototype of the A-5;
  • A-3/U2: experimental carrier of 73 mm RZ 65 rockets;
  • A-3/U3: reconnaissance plane with Rb 50/30 aerial cameras in the fuselage, armament reduced by the removal of the MG/FF cannons;
  • A-3/U4: reconnaissance aircraft with two Rb 12.5/7x9 aerial cameras mounted in the fuselage and an EK 16 gun camera or a Robot II miniature camera on the leading edge of the left wing. The armament was the same as the U3 version, with the addition of an ETC 501 bomb rack under the fuselage to carry a 300-liter fuel tank. 12 aircraft were produced;
  • A-3/U7: Prototype of a light high-altitude fighter, three built. It was characterized by its armament, consisting of only two MG 151/20E cannons in the fuselage, as well as the use of external supercharger intakes.

From February to August 1942, a total of 580 aircraft were produced, and from October 1942 to March 1943, under the "Hamburg" program, an export series of 75 Fw 190 A-3 aircraft was built for Turkey, in whose skies they coexisted peacefully with the Spitfires supplied by the British. On the Turkish planes, all cannons were replaced by machine guns.

The Fw 190 A-3 was most often used in battles over England and on the Eastern Front. One of these planes landed on a British airbase in June 1942 due to a navigational error by the pilot. Tests of the captured aircraft showed that the A-3 was superior to the Spitfire VB in maximum speed and rate of climb at all altitudes, as well as in acceleration characteristics. In a dive, the Fw 190 A-3 easily caught up with the Spitfire, and also had an advantage in maneuverability, except steady (serial) turns. After tests with all types of fighters in service with the Royal Air Force, it turned out that only the new Spitfire IX, which had just entered service, was able to fight on equal terms with the A-3.

Used sources:

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

2. “Wings of the Luftwaffe” Translation of V. Green’s book “Combat Aircraft of the Third Reich” by A. Firsov, 1993

3. A.N. Bear "Focke-Wulf FW190" Arsenal-Press, 1993

4. O. Rastrenin “Luftwaffe attack aircraft. Myths and Reality” journal. Aviation and Cosmonautics, No. 3, 2014

5. Materials from the site airwar.ru

Indicated stall speed in flight configuration: 166..189 km/h
Indicated stall speed in takeoff/landing configuration: 166..172 km/h
Dive speed limit: 850 km/h
Maximum load factor: 11 G
Stall angle of attack in flight configuration: 19.5°
Stall angle of attack in landing configuration: 18.1°
 
Maximum true air speed at sea level, engine mode - Emergency: 560 km/h
Maximum true air speed at 3000 m, engine mode - Emergency: 581 km/h
Maximum true air speed at 6400 m, engine mode - Emergency: 662 km/h
 
Maximum true air speed at sea level, engine mode - Combat: 535 km/h
Maximum true air speed at 3000 m, engine mode - Combat: 562 km/h
Maximum true air speed at 6000 m, engine mode - Combat: 626 km/h
 
Service ceiling: 10800 m
Climb rate at sea level: 16.0 m/s
Climb rate at 3000 m: 12.7 m/s
Climb rate at 6000 m: 10.3 m/s
 
Maximum performance turn at sea level: 23.0 s, at 280 km/h IAS.
Maximum performance turn at 3000 m: 28.0 s, at 280 km/h IAS.
 
Flight endurance at 3000 m: 3.2 h, at 350 km/h IAS.
 
Takeoff speed: 170..210 km/h
Glideslope speed: 205..215 km/h
Landing speed: 160..170 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 are given for Combat power, turn times are given for Emergency power.
 
Engine:
Model: BMW-801D
Maximum power in Emergency mode at sea level: 1700 HP
Maximum power in Emergency mode at 5700 m: 1440 HP
Maximum power in Combat mode at 700 m: 1520 HP
Maximum power in Combat mode at 5300 m: 1320 HP
 
Engine modes:
Nominal (unlimited time): 2300 RPM, 1.2 ata
Combat power (up to 30 minutes): 2400 RPM, 1.32 ata
Emergency power (up to 3 minutes): 2700 RPM, 1.42 ata
 
Oil rated temperature in engine intake: 60..70 °C
Oil maximum temperature in engine intake: 85 °C
Oil rated temperature in engine output: 105 °C
Oil maximum temperature in engine output: 120 °C
Cylinder head rated temperature: 180 °C
Cylinder head maximum temperature: 220 °C
Supercharger gear shift altitude: automatic
 
Empty weight: 3148 kg
Minimum weight (no ammo, 10% fuel): 3330 kg
Standard weight: 3855 kg
Maximum takeoff weight: 4385 kg
Fuel load: 409 kg / 524 l
Useful load: 1237 kg
 
Forward-firing armament:
2 x 20mm gun "MG 151/20", 250 rounds, 700 rounds per minute, synchronized
2 x 7.92mm machine gun "MG 17", 900 rounds, 1200 rounds per minute, synchronized
2 x 20mm gun "MG FF", 60 rounds, 540 rounds per minute, wing-mounted (modification)
2 x 20mm gun "MG FF", 90 rounds, 540 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"
500 kg general purpose bomb "SC 500"
 
Length: 8.85 m
Wingspan: 10.51 m
Wing surface: 18.3 m²
 
Combat debut: March 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. The engine supercharger has an automatic switch system which depends on altitude and engine revolutions.
- 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.
- When the angle of attack increases to critical levels the wing may stall suddenly and unexpectedly. There is almost no pre-stall buffet before the stalling. To avoid this the pilot must pay additional attention when performing extreme maneuvering.
- 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 which is electrically-actuated. It should be set to +1.5° before takeoff and 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 electrically-actuated landing flaps with three fixed positions: retracted, takeoff (13°) and landing (58°). Flaps control buttons and indicator lights are located on left panel near the throttle. The flap angle may also be checked by indicators on the left and right wing outside the cockpit.
- The aircraft has a tailwheel lock system which locks the tailwheel if the flight-stick is pulled backward. The tailwheel should be locked when taxiing straight for a long distance, before takeoff and after touchdown upon 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 remaining fuel in fuel tanks depending on switch position. In game the fuel indicator switch changes by pressing (RShift+I). Also, the airplane has an emergency fuel warning light (100 liters).
- It is impossible to open or close the canopy at high speed due to strong airflow. The canopy has an emergency release system for bailouts.
- The control system for the bomb rack only allows for dropping 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 radiator control handle: auto radiator 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 radiator control handle for various flight modes: auto radiator control
 
4. Approximate fuel consumption at 2000 m altitude:
- Cruise engine mode: 7.1 l/min
- Combat engine mode: 8.9 l/min
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