Fw 190 A-8 / IL-2 Sturmovik: Great Battles
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Fighter
Fw 190 A-8
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 the beginning of 1944, aircraft from the A-0 to A-7 series were delivered to combat units.

From the beginning of 1944, the problem of countering Allied bombers, which were now heavily escorted by fighters, became more acute. In March 1944, the British and Americans unexpectedly encountered the new Fw 190 A, which had more effective weapons and armor — it was an aircraft of the Fw 190 A-8 modification.

This aircraft differed from the previous modification of the A-7 by the installation of a "dry boost" system and an additional 115-liter fuel tank behind the cockpit, which made it possible to increase the aircraft's range. The pressurized air tank was moved to the right wing tip. The "dry boost" system, by installing an air pressure regulator in the pressure line of the engine, made it possible to increase the pressure and thus the power of the engine. As a result, the C3 injection system was discontinued.

The armament, as with the A-7 modification, included four cannons and two synchronized heavy machine guns.

On the A-8, the field modification kit nomenclature was partially revised:
  • A-8/R1: six 20 mm MG 151 cannons, four of which were mounted in pairs in two WB 151 mounts under the outer wing sections instead of two wing cannons. Production was soon discontinued;
  • A-8/R2: 30 mm MK 108 cannons instead of external wing-mounted MG 151/20s;
  • A-8/R3: even more powerful 30 mm MK 103 cannons under the wings. Production was soon discontinued;
  • A-6/R6: mounting of two Wfr.Gr.21 rockets;
  • A-8/R7: reinforced armored cockpit canopy (57 mm and 30 mm armored glass in front and the front side edges);
  • A-8/R8: similar to the previous variant, but with thicker armor in front of the cockpit and armor plates in front of the MK 108 wing cannon bays, mounted like the R2. External armor was also installed on the sides of the cockpit and 30 mm thick armored glass on the canopy, where the MG 131 machine guns were removed to reduce weight. Successful use in combat led to an order for mass production of the Fw 190 A-8/R8 "Ram" modification;
  • A-8/R11: night fighter-interceptor, Neptune or Liechtenstein radar installed;
  • A-8/R12: night fighter, a combination of R2 (MK 108 cannons instead of external wing MG 151/20) and R11 (radar).

In addition, a factory-modified A-8/U1 (or Fw 190 S-8), a two-seater trainer, was built to retrain fighter pilots from dive bombers to the Fw 190 (58 aircraft were built).

In addition to the main modification of the Fw 190 A-8, an attack version was produced, designated F-8. The external cannons were removed, and the external armament consisted of a ventral bomb rack capable of carrying up to a 1000 kg bomb, and four bomb racks under the wings. These aircraft were used by the so-called "Sonderstaffel Einhorn." A 1000 kg bomb could be carried specifically for attacks on high-value targets. Typically, F-8s carried a 250 or 500-kg bomb and four SD 70s under the wings.

There was also a bomber modification of the G-8, capable of carrying a 500 kg bomb or external tank under the fuselage and a 250 kg bomb under each wing.

The Fw 190 A-8 was a test aircraft for air-to-air missiles: wire-guided X-4 missiles were mounted under the wings.

The Fw 190 A-8 became the most-produced variant — 6,597 were produced before the end of the war, not counting the two-seat training, bomber, and attack versions.

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: 177..208 km/h
Indicated stall speed in takeoff/landing configuration: 164..188 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: 558 km/h
Maximum true air speed at 3000 m, engine mode - Emergency: 580 km/h
Maximum true air speed at 6200 m, engine mode - Emergency: 641 km/h
 
Maximum true air speed at sea level, engine mode - Combat: 532 km/h
Maximum true air speed at 3000 m, engine mode - Combat: 558 km/h
Maximum true air speed at 5800 m, engine mode - Combat: 612 km/h
 
Service ceiling: 10300 m
Climb rate at sea level: 13.8 m/s
Climb rate at 3000 m: 10.1 m/s
Climb rate at 6000 m: 7.8 m/s
 
Maximum performance turn at sea level: 24.2 s, at 280 km/h IAS.
Maximum performance turn at 3000 m: 33.0 s, at 280 km/h IAS.
 
Flight endurance at 3000 m: 3.8 h, at 350 km/h IAS.
 
Takeoff speed: 180..220 km/h
Glideslope speed: 215..225 km/h
Landing speed: 160..180 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: 3504 kg
Minimum weight (no ammo, 10% fuel): 3697 kg
Standard weight: 4391 kg
Maximum takeoff weight: 5239 kg
Fuel load: 498 kg / 639 l
Useful load: 1735 kg
 
Forward-firing armament:
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
2 x 13mm machine gun "MG 131", 475 rounds, 900 rounds per minute, synchronized
2 x 30mm gun "MK 108", 55 rounds, 650 rounds per minute, wing-mounted (modification)
 
Bombs:
Up to 8 x 66 kg fragmentation bombs "SD 70"
Up to 3 x 249 kg general purpose bomb "SC 250"
500 kg general purpose bomb "SC 500"
1090 kg general purpose bomb "SC 1000"
 
Rockets:
Two WGr.21 rockets in jettisonable launchers
Up to 12 Panzerblitz 1 rockets (R-HL, M8)
 
Length: 8.85 m
Wingspan: 10.51 m
Wing surface: 18.3 m²
 
Combat debut: Spring 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 engine supercharger has an automatic switch system which depends on altitude and engine revolutions.
- There is an additional emergency engine mode system installed. When it is engaged, the first supercharger gear pressure increases to 1.58 ATA and the second gear pressure to 1.65 ATA, the time limit is 10 minutes. This system is turned on by the engine boost command and works only when the throttle is set to 100%, automatic propeller pitch system is engaged and the altitude is lower than critical altitude for a given supercharger gear.
- 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 are located on left panel near the throttle. The flap angle may 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 standard bomb release controller (without modification) allows dropping the bombs only one by one. The strike modification (F-8) bomb release controller allows to choose the bomb release order for underbelly and underwing bombs and the delay between each bomb in the salvo.
- 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: 7.2 l/min
- Combat engine mode: 10.5 l/min
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