Il-2 mod.1943 / IL-2 Sturmovik: Great Battles
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Sturmovik
Il-2 mod.1943
History
Specifications

Developed by S.V. Ilyushin, the Il-2 attack plane became the main attack aircraft of Soviet aviation during the Great Patriotic War and at the same time the most-produced combat aircraft in the world.

The first flight of the two-seat BSh-2 (TsKB-55) armored attack aircraft took place in 1939, but even after modifications the aircraft did not meet the requirements of the technical specifications: it did not develop the required maximum speed and had an insufficient flight range. Therefore, the engine of the AM-35 high-altitude fighter was replaced by a specially designed AM-38 engine, the aircraft was converted into a single-seat version, the fuselage was lengthened, the canopy was changed, the armor on the rear hemisphere was reinforced, and an additional fuel tank was installed. The new aircraft, with the designation TsKB-57, took off for the first time on October 12, 1940, and went into mass production in March 1941.

In the early days of the war, it became clear that single-seat attack aircraft were suffering unreasonably high losses to enemy fighters, but there were strict orders not to slow down the rate of production of attack aircraft, which would of course have resulted from the introduction of a new two-seat modification into production. To reduce losses from enemy fighters, single-seat versions were handmade into two-seat versions in frontline formations.

Only at the end of 1942 did the Il-2 officially become a two-seater again. The gunner's cabin was outside the armored fuselage, directly behind the armored partition of the rear fuel tank. The gunner sat on a transverse canvas strap. He was shielded from above by a transparent canopy that folded to the side; from behind he was protected from enemy fire by a 6mm armored partition, while there was no protection from below or from the sides. The Berezin large-caliber turret machine gun was mounted on a half-turret installation and had firing angles of 35° up, 7° down, 25° to the left of the gunner, and 35° to the right. The increased load on the tail wheel forced an increase in its diameter and a strengthening of the fork design. The addition of a gunner's cockpit increased the weight of the attack aircraft by 270 kg, which slightly worsened its take-off characteristics and longitudinal stability. To reduce the takeoff distance, a 17° flap angle was introduced, allowing this parameter to be maintained. Longitudinal stability was improved thanks to new wings with a sweep angle of 15° along the leading edge. However, the increased weight of the aircraft made it difficult to control and maneuver, which necessitated the installation of a more powerful engine to increase power. The Mikulin design bureau created a boosted version of the AM-38F with a take-off power of 1,720 hp. The time of continuous operation in takeoff mode was limited to 5 minutes, and the rated power at a design altitude of 750 m was 1575 hp.

Since February 1943 only this modification was produced. The installation of a more powerful engine increased the maximum speed and rate of climb on the ground, while the lower altitude of the engine reduced the maximum flight speed at altitude, which was uncritical for an attack aircraft operating mainly at low altitudes. The take-off characteristics of the attack aircraft increased significantly and, with a bomb load of 400 kg, proved to be practically equal to the take-off characteristics of the single-seat Il. However, the 1943 modification of the Il-2 differed from previous models not only by the installation of a new engine. The tanks inside the fuselage were protected by fiberglass, which improved the protection of the aircraft. From 1944, the aircraft was equipped with a metal wing with a modified sweep along the leading edge, which improved controllability.

Il-2 attack aircraft of the 1943 model were produced almost until the last year of the war, gradually being replaced in production by new aircraft of the Il-10 type.

The undoubted advantages of the IL-2 design are expressed in its excellent performance characteristics: high reliability and maintainability. The aircraft was extremely unpretentious at all stages of flight preparation and execution. "It was one of the most accessible aircraft to master," wrote the two-time Hero of the Soviet Union, Air Marshal A.N. Efimov, in his memoirs. - Flying itself was not difficult. When flying over a target or in a dogfight, the pilot's attention was not distracted by complex manipulations of instruments and assemblies in the cockpit. The plane forgave the pilot even gross mistakes in piloting, which was very important in carrying out attacks and fighting when there was no time to watch the instruments. "I don't know of a single case where an aircraft lost control or went into a dive due to pilot error.

1. E. Chernikov “Armored attack aircraft Il-2” M-Hobby 1998

2. V. Perov, O. Rastrenin “Il-2 Sturmovik”, Aviation and Cosmonautics magazine No. 5-6 2001

3. Materials from the site airwar.ru

Indicated stall speed in flight configuration: 144..159 km/h

Indicated stall speed in takeoff/landing configuration: 135..152 km/h
Dive speed limit: 570 km/h
Maximum load factor: 10.5 G
Stall angle of attack in flight configuration: 19.4 °
Stall angle of attack in landing configuration: 17.5 °
 
Maximum true air speed at sea level, engine mode - Boosted: 407 km/h
Maximum true air speed at sea level, engine mode - Nominal: 389 km/h
Maximum true air speed at 1200 m, engine mode - Nominal: 400 km/h
 
Service ceiling: 5600 m
Climb rate at sea level: 7.5 m/s
Climb rate at 3000 m: 4.2 m/s
 
Maximum performance turn at sea level: 26.6 s, at 250 km/h IAS.
Maximum performance turn at 3000 m: 39.3 s, at 250 km/h IAS.
 
Flight endurance at 3000 m: 1.4 h, at 300 km/h IAS.
 
Takeoff speed: 160..200 km/h
Glideslope speed: 195..205 km/h
Landing speed: 145..155 km/h
Landing angle: 11.7 °
 
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 Nominal power, turn times are given for Boosted power.
 
Engine:
Model: AM-38F
Maximum power in Boosted mode at sea level: 1720 HP
Maximum power in Nominal mode at sea level: 1500 HP
Maximum power in Nominal mode at 750 m: 1500 HP
 
Engine modes:
Nominal (unlimited time): 2050 RPM, 1200 mm Hg
Boosted power (up to 5 minutes): 2350 RPM, 1360 mm Hg
 
Water rated temperature in engine output: 80..110 °C
Water maximum temperature in engine output: 120 °C
Oil rated temperature in engine intake: 40..80 °C
Oil maximum temperature in engine intake: 85 °C
Oil rated temperature in engine output: 115 °C
Oil maximum temperature in engine output: 120 °C
 
Supercharger gear shift altitude: single gear
 
Empty weight: 4715 kg
Minimum weight (no ammo, 10% fuel): 5014 kg
Standard weight: 5681 kg
Maximum takeoff weight: 6375 kg
Fuel load: 535 kg / 730 l
Useful load: 1660 kg
 
Forward-firing armament:
2 x 20mm gun "SsVAK", 250 rounds, 800 rounds per minute, wing-mounted
2 x 7.62mm machine gun "ShKAS", 750 rounds, 1800 rounds per minute, wing-mounted
2 x 23mm gun "VYa-23", 150 rounds, 600 rounds per minute, wing-mounted (modification)
2 x 37mm gun "NS-37", 50 rounds, 250 rounds per minute, wing-mounted (modification)
 
Defensive armament:
Backward: 12.7 mm machine gun "UBT", 150 rounds, 1000 rounds per minute (modification)
 
Bombs:
Up to 240 x 1.5 kg HEAT bomblets "PTAB-2,5-1,5"
Up to 6 x 50 kg general purpose bombs "FAB-50sv"
Up to 6 x 104 kg general purpose bombs "FAB-100M"
2 x 254 kg general purpose bombs "FAB-250sv"
 
Rockets:
4 x 7 kg rockets "ROS-82", HE payload mass 2.5 kg
4 x 15 kg rockets "RBS-82", HEAT payload mass 7.2 kg
4 x 42 kg rockets "ROFS-132", HE payload mass 21.3 kg
 
Length: 11.5 m
Wingspan: 14.6 m
Wing surface: 38.5 m²
 
Combat debut: early 1943
 
Operation features:
- The engine has a boost mode which is engaged by setting mixture control lever to maximum position.
- The engine has a single stage mechanical supercharger which does not require manual control.
- Engine mixture control is automatic when the mixture lever is set to the intermediate (50%) position. It is possible to manually lean the mixture by moving the control lever to less than 50%. This will lower fuel consumption during flight.
- Engine RPM has an automatic governor and it is maintained at the required RPM corresponding to the governor control lever position. The governor automatically controls the propeller pitch to maintain the required RPM.
- Water and oil radiator shutter control is manual. Airplane has armoured oil radiator shutters which should be closed at the beginning of ground attack to reduce a possibility of combat damage. After finishing the attack, it is necessary to re-open the shutters to the required position.
- The aircraft has only the pitch flight-control trimmer.
- Landing flaps have a pneumatic actuator. Flaps can be extended fully or to takeoff position - 17°, gradual extending is impossible. Due to the weak force of the actuator the extended landing flaps may be pressed upwards by the airflow if the airspeed is more than 220 km/h. Remember that the flaps will not extend fully in case of high speed. In case of a high-speed landing approach the flaps may extend a few steps further right before the landing which will cause the aircraft to shoot upwards.
- The aircraft has a manual tailwheel lock. Wheel should be locked when taxiing straight for a long distance and before takeoff and landing.
- The aircraft has differential pneumatic wheel brakes with shared control lever. This means that if the brake lever is held and the rudder pedal the opposite wheel brake is gradually released causing the plane to swing to one side or the other.
- The aircraft has a fuel gauge which shows the amount of remaining fuel in the front or bottom fuel tank depending on switch position. In game the fuel indicator switch changes by pressing (RShift+I). Rear fuel tank level is not indicated. 
- Cockpit canopy weight is 50 kg and it has no lock in the open position, for this reason the canopy may to spontaneously close in a deep dive. Also, it is impossible to open or close canopy at high speed due to strong airflow. The canopy has no emergency release, so bail out requires the speed drop before it.
- The aircraft is equipped with a joint salvo controller both for bombs and rockets, it has three release/fire modes: single launch, launch two in a salvo or launch four in a salvo.
- The mechanical gun sight "Visier Vladimirova" allows aiming rockets and guns at ground and air targets and horizontal bombing at certain speeds and altitudes.
 
Basic data and recommended positions of the aircraft controls:
1. Starting the engine:
- recommended position of the mixture control lever: 50% (auto mixture control)
- recommended position of the radiators control handles: close
- recommended position of the prop pitch control handle: 100%
- recommended position of the throttle lever: 10%
- before taxiing, you must unlock the tailwheel
 
2. Recommended mixture control lever positions for various flight modes: 50% (auto mixture control)
 
3.1 Recommended positions of the oil radiator control handle for various flight modes:
- takeoff: open 100%
- climb: open 100%
- cruise flight: open 50-60%
- combat: close (to prevent combat damage)
 
3.2 Recommended positions of the water radiator control handle for various flight modes:
- takeoff: open 100%
- climb: open 100%
- cruise flight: open 60-70%
- combat: open 100%
 
4. Approximate fuel consumption at 2000 m altitude:
- Cruise engine mode: 9.6 l/min
- Combat engine mode: 11.4 l/min
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