Fw 190 A-5 / IL-2 Sturmovik: Great Battles
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Fighter
Fw 190 A-5
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 fall of 1940 to 1942, aircraft from the A-0 to A-4 series were delivered to combat units.

In November 1942, a new version of the Fw 190 A-5 fighter went into production. The prototype for the A-5 was a modified version of the A-3/U1, in which the forward section of the fuselage was lengthened by 150 mm, which significantly improved controllability. The armament remained the same: 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 attack modifications were equipped with a system to increase the power of the engine, using an additional injection of C-3 fuel (with 96 octane) for a short-term emergency increase in maximum speed at altitudes below 1000 m.

The Fw 190 A-5 had many modifications, some of which remained at the prototype level:
  • A-5/U2: night fighter-bomber with extended range. It had anti-reflective strips on the engine exhausts, a bomb rack under the fuselage, and two Messerschmitt bomb racks under the wings for 300-liter drop tanks. Armament: two MG 151/20 cannons. Later designated Fw 190 G-2/N;
  • A-5/U3: attack aircraft (fighter-bomber) also without MG/FF cannons. It had three bomb racks — one under the fuselage for 500 kg bombs and two under the wings for 250 kg bombs, as well as additional armor. Later the designation was changed to Fw 190 F-2. There was also a tropical version, the A-5/U3/trop (F-2trop);
  • A-5/U4: fighter-reconnaissance aircraft with two Rb 12.5/7x9 aerial cameras and without MG/FF cannons. There was also a tropical version A-5/U4/trop;
  • A-5/U8: Extended range fighter-bomber with ETC 501 bomb rack under the fuselage. Prototype for the G-1 series (equipped with Junkers underwing racks for 300-liter drop tanks) and G-2 (equipped with Messerschmitt racks). Armament: two MG 151/20 cannons in the wing root;
  • A-5/U9: experimental version with MG 131 heavy machine guns instead of MG 17 and MG 151/20 cannons instead of MG/FF. Two built;
  • A-5/U10: experimental version with MG 151 cannons in the outer wing instead of MG/FF. Two were built and became prototypes for later production;
  • A-5/U11: experimental version, equipped with 30 mm MK 103 outboard cannons instead of MG/FF cannons. One prototype was built — this variant was later used in the R3 Field Development Kit;
  • A-5/U12: with two gunpods, each with a pair of MG 151/20 cannons instead of MG/FF cannons, for a total of six cannons. Two aircraft were built;
  • A-5/U13: with autopilot. Three aircraft were built which became prototypes for the G-3 model;
  • A-5/U14 and A-5/U15: experimental torpedo fighter variants. One aircraft was built. After the tests ended with unsatisfactory results, U15 was used for experiments with the BV 246 glide bomb;
  • A-5/U16: instead of MG/FFs, 30 mm MK 108 cannons were installed in the outer wing for attacks on bomber formations. One aircraft was built, this weapon variant was later used for the R2 kit;
  • A-5/U17: attack aircraft, prototype for the F-3/R1 series with one ETC 501 bomb rack under the fuselage and four ETC 50s under the wings for 50 kg bombs.
With the previous modification of the A-4, field modification kits appeared for the first time for this type of fighter:
  • A-5/R3: with 30 mm MK 103 external cannons instead of MG/FF cannons.
  • A-4/R6 (similar to the A-4 modification): a fighter armed with two Wfr.Gr.21 unguided rockets. Such vehicles were called "Formation Destroyers" in the Luftwaffe. These 210 mm rockets were first used in the summer of 1943. The experiment was considered successful, but the number of enemy aircraft hit by the projectiles was small since the projectile had a remote fuse that was set on the ground. In combat, pilots had difficulty in determining the distance to the target and inaccurately chose the necessary lead: it was calculated that the destruction of part of the group's bombers by shrapnel would force them to change course and disrupt the battle formation, and the fighters, having jettisoned their rocket launchers, would then enter the battle with their cannons.

Another A-5/R6 was tested with 280 mm Wfr.Gr.28 rockets, which was unsuccessful.

Between November 1942 and June 1943, 1,752 fighters of the A-5 modification were produced.

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: 169..195 km/h
Indicated stall speed in takeoff/landing configuration: 160..175 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: 578 km/h
Maximum true air speed at 6400 m, engine mode - Emergency: 658 km/h
 
Maximum true air speed at sea level, engine mode - Combat: 533 km/h
Maximum true air speed at 3000 m, engine mode - Combat: 558 km/h
Maximum true air speed at 6000 m, engine mode - Combat: 622 km/h
 
Service ceiling: 10600 m
Climb rate at sea level: 15.4 m/s
Climb rate at 3000 m: 11.9 m/s
Climb rate at 6000 m: 9.7 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: 3219 kg
Minimum weight (no ammo, 10% fuel): 3401 kg
Standard weight: 3926 kg
Maximum takeoff weight: 4648 kg
Fuel load: 409 kg / 524 l
Useful load: 1429 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", 90 rounds, 540 rounds per minute, wing-mounted (modification)
4 x 20mm gun "MG 151/20", 125 rounds, 700 rounds per minute, wing-mounted (modification)
 
Bombs:
Up to 8 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: Spring 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.
- U17 strike 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% 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.
- 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: 6.9 l/min
- Combat engine mode: 10.5 l/min
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