Fw 190 D-9 / IL-2 Sturmovik: Great Battles
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Fighter
Fw 190 D-9
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.

During the war, modifications of fighter planes with high-altitude engines were developed, one of which was the Fw 190 D version with the Jumo 213 engine — the first tests were conducted as early as March 1942. Allied air raids delayed the introduction of this engine into serial production, which began in mid-1944. The "long-nose" modification of the Fw 190 D-9, the "Dora-9," went into mass production at the same time.

The water-cooled Jumo 213 engine was a further development of the 1936 Jumo 211 engine but was smaller and produced more power. The Jumo 213 AG had a takeoff power of 1900 hp, and the MW 50 system made it possible to raise it to 2240 hp for 10 minutes when the altitude decreased from 5500 m to 4750 m. At high altitudes, the GM-1 boost system was planned, but in reality, unlike the MW 50, it was not used. The engine was mounted on a lengthened engine frame, and a ring-type radiator with adjustable flaps was located in the nose.

The pilot's cockpit and two main fuel tanks were located in the center of the fuselage. The tail section housed the rest of the equipment, and the tail unit was attached by a special insert that balanced the elongated engine.

The aircraft repeated the design solutions of the Fw 190 A-9 modification, but the load-bearing elements of the fuselage were strengthened. The armament consisted of two MG 151/20 cannons in the wing roots and two synchronized machine guns. An ETC 501 (or an ETC 504) bomb rack was mounted under the fuselage to carry a 250 kg bomb or a 300-liter drop tank.

The Fw 190 D-9 had several field modification kits, of which only the R5 and R11 kits were in use. The other kits were not mass-produced:
  • D-9/R1: two MG 131 machine guns in the fuselage and four 20 mm MG 151/20 cannons installed under the outer wing sections;
  • D-9/R2: 30 mm MK 108 cannon instead of 20 mm MG 151/20;
  • D-9/R5: fighter-bomber with ETC 50 or 71 underwing racks;
  • D-9/R6: two 21 cm WGr rockets under the wings for operations against large bomber formations;
  • D-9/R11 - all-weather fighter. It was equipped with a PKS 12 autopilot, FuG 16Za, FuG 25a, and FuG 125 radio equipment (a radio navigation device that allowed a "blind" landing), as well as an LGWK 23 anti-icing device;
  • D-9/R14 - a torpedo bomber that could carry one LT 1B torpedo (LTF 56) or one BT 1400 torpedo bomb, suspended from a standard ETC 504 mount using an adapter. Development of this modification was canceled;
  • D-9/R20 - equipped with the MW 50 system. During production the D-9 received this system as standard, so the designation was not used;
  • D-9/R21 - a combination of R11 and R20 - an all-weather fighter with an engine equipped with the MW 50 system;
  • D-9/R25: variant with the Jumo 213 ZEV engine, with the same equipment as the R11 and R20. An additional fuel tank at the rear of the fuselage and two tanks in the wing for the MW 50 system. It was planned that this version would be put into production in July - August 1945, but for obvious reasons it was not possible to do this in time.

A total of 1,805 Fw 190 D-9 aircraft were produced.

Initially, fighter pilots were critical of the new machine, but after becoming familiar with it, they could see many clear advantages over the Fw 190 A and Bf 109, including a very high dive speed and good climb rate. The maximum flight speed at an altitude of 6500 m was 685 km/h, and in the maximum boost mode of the engine with MW 50 it increased by another 15 - 20 km/h: now the Germans could reach speeds comparable to those of the American Mustang. It is true that with an increase in altitude to 8000 m, the speed of the D-9 dropped sharply, making it difficult to conduct battles at that altitude.

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: 174..197 km/h
Indicated stall speed in takeoff/landing configuration: 160..181 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: 607 km/h
Maximum true air speed at 2000 m, engine mode - Emergency: 641 km/h
Maximum true air speed at 5200 m, engine mode - Emergency: 694 km/h
 
Maximum true air speed at sea level, engine mode - Combat: 565 km/h
Maximum true air speed at 3200 m, engine mode - Combat: 623 km/h
Maximum true air speed at 6500 m, engine mode - Combat: 663 km/h
 
Service ceiling: 11600 m
Climb rate at sea level: 19.0 m/s
Climb rate at 3000 m: 17.3 m/s
Climb rate at 6000 m: 14.6 m/s
 
Maximum performance turn at sea level: 20.0 s, at 300 km/h IAS.
Maximum performance turn at 3000 m: 29.0 s, at 300 km/h IAS.
 
Flight endurance at 3000 m: 2.5 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: Jumo-213 A1
Maximum power in Emergency mode at sea level: 2130 HP
Maximum power in Emergency mode at 3800 m: 1980 HP
Maximum power in Combat mode at sea level: 1900 HP
Maximum power in Combat mode at 5100 m: 1680 HP
 
Engine modes:
Nominal (unlimited time): 3000 RPM, 1.42 ata
Combat power (up to 30 minutes): 3250 RPM, 1.51 ata
Emergency power (up to 3 minutes): 3250 RPM, 1.7 ata
Emergency power with MW-50 (up to 10 minutes): 3250 RPM, 1.8 ata
 
Water rated temperature in engine output: 55..100 °C
Water maximum temperature in engine output: 110 °C
Oil rated temperature in engine output: 40..110 °C
Oil maximum temperature in engine output: 120 °C
 
Supercharger gear shift altitude: automatic
 
Empty weight: 3443 kg
Minimum weight (no ammo, 10% fuel): 3759 kg
Standard weight: 4289 kg
Maximum takeoff weight: 4832 kg
Fuel load: 388 kg / 524 l
Useful load: 1389 kg
 
Forward-firing armament:
2 x 20mm gun "MG 151/20", 250 rounds, 700 rounds per minute, wing-mounted
2 x 13mm machine gun "MG 131", 475 rounds, 900 rounds per minute, synchronized
 
Bombs:
Up to 4 x 66 kg fragmentation bombs "SD 70"
249 kg general purpose bomb "SC 250"
500 kg general purpose bomb "SC 500"
 
Rockets:
Two WGr.21 rockets in jettisonable launchers
26 R4M rockets
 
Length: 10.2 m
Wingspan: 10.51 m
Wing surface: 18.3 m²
 
Combat debut: end of September 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.
- The aircraft is equipped with MW-50 water-methanol mixture injection system that prevents the engine detonation in the emergency power mode.
- Radiator flaps are controlled automatically, keeping a set coolant temperature. This temperature can be set by a pilot using the thermostat regulator if needed (default 0% setting is adequate for all engine modes, while increasing it cools the engine more).
- 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 allows dropping the bombs only 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%
 
2. Recommended mixture control lever positions for various flight modes: auto mixture control
 
3. Recommended positions of the cowl flap control handle (thermostat controls) for various flight modes:
- takeoff: open 50%
- climb: open 100%
- cruise flight: open 70%
- combat: open 100%
 
4. Approximate fuel consumption at 2000 m altitude:
- Cruise engine mode: 9.7 l/min
- Combat engine mode: 11.2 l/min
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