Il-2 mod.1941 / IL-2 Sturmovik: Great Battles
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Sturmovik
Il-2 mod.1941
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.

The Il-2 circa. 1941 was a single-seat, single-engine, all-metal, low-wing aircraft with retractable landing gear and a tail wheel. The pilot, engine, and fuel tanks were protected by a 4-8 mm armored hull, and the total weight of the armor was 780 kg. The wing and rear fuselage were attached to the armored hull, the strongest element of the airframe. The first series of the Il-2 did not have armor protection over the pilot's head, engine, or rear fuel tank, as it was assumed that enemy fighters would not be able to effectively attack the fighter from above. The tail section of the fuselage and the wings of this series were made entirely of metal, but even at the design stage, it was possible to replace part of the metal structure with wood.

The engine was a water-cooled AM-38 with a variable-pitch propeller. Offensive weapons included 2 machine guns and 2 cannons in the wing. The 20 mm cannons were located closer to the fuselage in the all-metal wings. The 1941 model had no defensive weapons. In addition to small arms and cannons, the aircraft could carry up to 8 unguided rockets and up to 600 kg of bombs.

A total of 8,360 single-seat Il-2s were produced, including up to 6,000 with 23 mm VYa cannons.

In the early days of the war, it became clear that single-seat attack aircraft were suffering disproportionately high losses to enemy fighters. The engineering and technical staff of the regiments, with input from the pilots, began to find ways to protect the aircraft from fighters. Typically, the rear fairing of the cockpit canopy was removed to place a gunner and machine gun with minimal ammunition behind the fuel tank.

It also turned out that the "armored" plane was being hit even by 20 mm anti-aircraft guns — the armor protected only against bullets — but others did not have such protection. It should be noted that the saturation of mobile German units with anti-aircraft artillery was very high.

At the beginning of the war, it was extremely difficult to fight German tanks with the Il-2. The effectiveness of the 20 mm ShVAK cannons against tank armor was low, and it was impossible to drop bombs accurately from the Il-2: the pilot's gun sight proved to be ineffective, since the Il-2 attacked from low altitudes or in a very shallow dive, and the long canopy of the aircraft simply blocked the pilot's target, and during an emergency landing pilots were often injured by hitting their heads on the sight. For these reasons, the PBP-16 sight was removed from most of the Il-2 combat units, and cannon fire was carried out after zeroing with machine guns. Later the so-called Vasiliev BB-1 sight was used. It consisted of a reticle printed on armored glass and a sight on a pin mounted on the engine cowling. For bombing from horizontal flight, special markings were used on the cowl and the armored glass — by combining the markings, the pilot could approximately determine the moment of bomb release.

Despite all the difficulties and design flaws, the single-seat Il-2s attacked enemy motorized and armored columns rushing east, often without fighter cover. This slowed the German onslaught and reduced their offensive capabilities.

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: 136..156 km/h
Indicated stall speed in takeoff/landing configuration: 128..146 km/h
 
Dive speed limit: 570 km/h
Maximum load factor: 11.5 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: 430 km/h
Maximum true air speed at sea level, engine mode - Nominal (at 2150 RPM): 421 km/h
Maximum true air speed at 2500 m, engine mode - Nominal (at 2150 RPM): 455 km/h
 
Service ceiling: 7500 m
Climb rate at sea level: 9.4 m/s
Climb rate at 3000 m: 8.9 m/s
Climb rate at 6000 m: 3.9 m/s
 
Maximum performance turn at sea level: 23.1 s, at 250 km/h IAS.
Maximum performance turn at 3000 m: 32.6 s, at 250 km/h IAS.
 
Flight endurance at 3000 m: 1.7 h, at 300 km/h IAS.
 
Takeoff speed: 150..190 km/h
Glideslope speed: 185..195 km/h
Landing speed: 130..140 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-38
Maximum power in Boosted mode at sea level: 1600 HP
Maximum power in Nominal mode at sea level: 1500 HP
Maximum power in Nominal mode at 1650 m: 1500 HP
 
Engine modes:
Nominal (unlimited time): 2050 RPM, 1180 mm Hg
Boosted power (up to 10 minutes): 2150 RPM, 1280 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: 4242 kg
Minimum weight (no ammo, 10% fuel): 4464 kg
Standard weight: 5049 kg
Maximum takeoff weight: 5888 kg
Fuel load: 470 kg / 641 l
Useful load: 1646 kg
 
Forward-firing armament:
2 x 20mm gun "SsVAK", 210 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)
 
Bombs:
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:
8 x 7 kg rockets "ROS-82", HE payload mass 2.5 kg
8 x 15 kg rockets "RBS-82", HEAT payload mass 7.2 kg
8 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: June 1941
 
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 only be fully extended; 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 landing.
- 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 gunsight is installed on a sliding bar which allows the pilot to extend the gunsight towards the pilot allowing for an increase in the field of view through the gunsight.
 
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 50-60%
- combat: open 100%
 
4. Approximate fuel consumption at 2000 m altitude:
- Cruise engine mode: 8.7 l/min
- Combat engine mode: 10.0 l/min
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