Fw 190 A-6 / IL-2 Sturmovik: Great Battles
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Fighter
Fw 190 A-6
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 engine and a large convex cockpit canopy with a minimum of metal binding parts. The aircraft was characterized by good controllability and low stick loading. From the autumn of 1940 to 1943, aircraft from the A-0 to A-5 series were delivered to combat units.

In the spring of 1943, the ever-increasing takeoff weight of the aircraft began to affect its performance. It was decided to change the armament, for which the wing design was changed. The new wing was tested on Fw 190 A-5/U10 No. 861, which became the prototype for the new series.

The start of production of the Fw 190 A-6 series was planned for April 1943, but massive Allied air raids delayed it until late May - early June. The A-6 was distinguished by a new wing, in the outer part of the wings MG 151/20 cannons were mounted — for this, it was necessary to create convex fairings on the underside of the aircraft. The aircraft were equipped with reinforced wheels of the main landing gear and a Robot camera gun. If necessary, all A-6 series aircraft could be equipped with an ETC 501 bomb rack, which together with the ER 4 adapter beam made it possible to carry four SC 50 (SD 70) bombs.

The only factory modification of this model was the A-6/U3 attack aircraft (fighter-bomber), which entered service with "assault" detachments and groups. It had three bomb racks, one ventral for 500 kg bombs and two underwing for 250 kg bombs, as well as additional armor. Attack modifications were equipped with a system to increase engine power, using an additional injection of C3 fuel (with 96 octane) for a short-term emergency increase in maximum speed at altitudes below 1000 m.

The list of modifications to the A-6 was also slightly modified:
  • A-6/R1: armed with six MG 151/20 cannons, four of which were mounted in pairs in two WB 151 mounts under the wings instead of two wing cannons. 60 aircraft were converted;
  • A-6/R2: instead of the external wing MG 151/20, 30 mm MK 108 cannons were installed (built into the wing, as opposed to the A-5/U16). Not mass-produced;
  • A-6/R3: even more powerful (and heavier) 30 mm MK 103 cannons under the wings. Not mass-produced;
  • A-6/R6: the variant which, like the A-4 and A-5, provided for the mounting of two Wfr.Gr.21 rockets. 21 aircraft produced;
  • A-6/R2/R6: "formation destroyer", armed with two MG 17 machine guns, two 20 mm MG 151/20 E cannons, two 30 mm MK 108 cannons, and two Wfr.Gr. 21. Only one prototype built.
  • A-6/R7: armored version with conventional weapons, used in the Reich's air defense. A belly mount for a 300-liter fuel tank was often installed.
  • A-6/R8: Version with armament like the R2 (MK 108 cannon) and armor like the R7. The MG 17 machine guns were often removed. It was used for air defense and showed good effectiveness against American bombers;
  • A-6/R11: all-weather and night fighter-interceptor, sometimes with the installation of a FuG 217 Neptune radar. Typically, these aircraft used jettisonable fuel tanks mounted on an ETC 501 bomb rack;
  • A-6/R12: experimental version, a combination of R2 and R11.

A total of 1,192 Fw 190 A-6s were built.

Since the BMW 801D-2 engine was already considered unsatisfactory in terms of altitude, the A-6 was originally intended to be used as an attack aircraft. However, the aggravated situation in the skies over Germany forced us to reconsider this decision, and many Fw 190 A-6s were sent to fighter units.

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: 170..197 km/h
Indicated stall speed in takeoff/landing configuration: 156..178 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: 563 km/h
Maximum true air speed at 3000 m, engine mode - Emergency: 585 km/h
Maximum true air speed at 6400 m, engine mode - Emergency: 661 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: 560 km/h
Maximum true air speed at 6000 m, engine mode - Combat: 622 km/h
 
Service ceiling: 10400 m
Climb rate at sea level: 15.0 m/s
Climb rate at 3000 m: 11.3 m/s
Climb rate at 6000 m: 8.9 m/s
 
Maximum performance turn at sea level: 23.5 s, at 280 km/h IAS.
Maximum performance turn at 3000 m: 35.5 s, at 280 km/h IAS.
 
Flight endurance at 3000 m: 3.0 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: 3371 kg
Minimum weight (no ammo, 10% fuel): 3553 kg
Standard weight: 4140 kg
Maximum takeoff weight: 4766 kg
Fuel load: 409 kg / 524 l
Useful load: 1395 kg
 
Forward-firing armament:
2 x 7.92mm machine gun "MG 17", 900 rounds, 1200 rounds per minute, synchronized
2 x 20mm gun "MG 151/20", 250 rounds, 700 rounds per minute, synchronized
2 x 20mm gun "MG 151/20", 140 rounds, 700 rounds per minute, wing-mounted
 
Bombs:
Up to 8 x 66 kg general purpose bombs "SD 70"
Up to 3 x249 kg general purpose bomb "SC 250"
500 kg general purpose bomb "SC 500"
 
Rockets:
Two WGr.21 rockets in jettisonable launchers
 
Length: 8.85 m
Wingspan: 10.51 m
Wing surface: 18.3 m²
 
Combat debut: Summer 1943
 
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.
- G-3 and G-3/R-5 modification includes C3 additional fuel injection system. When engaged, it increases pressure to 1.65 ATA (10 minutes time limit). This system can be turned on by engine boost command only at 100%25 throttle, with automatic prop pitch control enabled and at altitudes lower than 1 km.
- Outlet cowl shutters are operated manually.
- 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. With "G-3" and "G-3/R-5" modifications it is possible to select left, right or both underwing bomb racks, but the centerline bomb rack is always selected and each push of the bomb release control will drop one of its bombs.
- 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 cowl flap 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. Recommended positions of the cowl flap control handle for various flight modes:
- takeoff: open 50%
- climb: open 100%
- cruise flight: open 30%
- combat: open 70%
 
4. Approximate fuel consumption at 2000 m altitude:
- Cruise engine mode: 7.1 l/min
- Combat engine mode: 10.5 l/min
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