MiG-3 ser.24 / IL-2 Sturmovik: Great Battles
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Fighter
MiG-3 ser.24
History
Specifications

The preliminary design of the I-200 front-line fighter was developed at the Polikarpov Design Bureau for the Mikulin AM-37 engine. However, when a design bureau assigned by the OKB and headed by Mikoyan and Gurevich began a detailed study of the project in 1939, the AM-37 was never completed. As a result, the AM-35A high-altitude engine, designed for use on long-range high-altitude bombers, was installed on the aircraft, and the aircraft was transformed into a high-altitude fighter. On April 5, 1940, the I-200 prototype was flown for the first time. Given the name MiG-1, the aircraft was put into mass production, but the flight range was considered insufficient by the leadership of the Soviet Air Force, and a new modification, the MiG-3, was developed. To increase the range, a 250-liter fuel tank was installed in the fuselage, while the AM-35A engine was moved forward to maintain alignment, but the changes somewhat worsened the aircraft's controllability.

The MiG-3 of the 24th series was a single-engine, single-seat, low-wing monoplane. The design of the plane was of mixed construction: the front part of the fuselage and the middle section were made of metal, and the rear part of the fuselage and the wings were made of wood. The fin was all metal, the tail was wooden, and the rudders were covered with canvas. The landing gear consisted of two main legs with a tail unit, retractable in flight. The aircraft was divided into complete structural and production units. Removable wings, a removable fuselage, and a landing gear with very simple kinematics allowed parallel assembly of the units on different stands and convenient assembly on a conveyor belt. The AM-35A liquid-cooled engine with an AV-5L-123 propeller developed 1350 hp in takeoff mode and 1200 hp in nominal mode at an altitude of 6000 m. To improve stability and flight safety, the capacity of the rear fuselage tank was reduced to 140 liters. As a result, the aircraft was easier to control during takeoff, turns, and landings, the takeoff run length was reduced, and climb stability was slightly improved.

The armament consisted of one large-caliber and two rifle-caliber machine guns. If necessary, bombs or unguided rockets could be carried under the wings.

MiG-3s of the 24th series arrived at the front in July 1941. At the beginning of the war, MiGs formed a significant part of the fighter fleet of the Western Military Districts, but unfortunately, the pilots did not have time to master these machines before the war, as a result, their losses amounted to almost 75% in the first days. But even in those terrible days, the MiG-3 showed what it could do in the right hands. Perhaps the first victory of a Soviet pilot in the war was won with it: political instructor Sokolov from the 129th IAP announced the downing of a German plane already at 4 am on June 22. On June 26, the future famous ace, and three-time Hero of the Soviet Union Alexander Pokryshkin shot down his first Messerschmitt in a MiG-3. Despite some successes, the combat use of the MiG-3 in front-line aviation was not very effective.

It performed much better in air defense units. These regiments, manned by experienced pilots, suffered less from accidents and disasters. Thanks to their training, their pilots could fight successfully day and night, and in air defense, the altitude of the fighter was necessary, since German bombers preferred to fly at high altitudes to protect themselves from anti-aircraft fire. By December 1941, MiG-3s accounted for more than a third of the air defense fighters, but after the production of the aircraft was discontinued (such engines were needed for the mass production of Il-2 attack aircraft), their number gradually began to decline. The ingenious design of the aircraft allowed the technical staff to assemble one from several defective aircraft directly on the airfield: the last MiGs were written off only in June 1944 due to wear and tear and lack of spare parts. According to official Soviet data, MiG-3 pilots shot down 710 enemy aircraft during the war, 43 of them at night. This is the highest result of all types of Soviet air defense fighters.

Used sources:

1. S. Ivanov “MiG-3” War in the air, No. 115 2004

2. V. Shavrov “History of aircraft designs in the USSR 1938-1950.” 1988

3. Materials from the site airwar.ru

Indicated stall speed in flight configuration: 159..175 km/h
Indicated stall speed in takeoff/landing configuration: 134..147 km/h
Dive speed limit: 750 km/h
Maximum load factor: 12.8 G
Stall angle of attack in flight configuration: 17.3 °
Stall angle of attack in landing configuration: 15.1 °
 
Maximum true air speed at sea level, engine mode - Boosted: 525 km/h
Maximum true air speed at sea level, engine mode - Nominal: 493 km/h
Maximum true air speed at 7600 m, engine mode - Nominal: 626 km/h
 
Service ceiling: 11800 m
Climb rate at sea level: 15.9 m/s
Climb rate at 3000 m: 14.0 m/s
Climb rate at 6000 m: 10.2 m/s
 
Maximum performance turn at sea level: 22.4 s, at 270 km/h IAS.
Maximum performance turn at 3000 m: 28.7 s, at 270 km/h IAS.
 
Flight endurance at 3000 m: 2.5 h, at 350 km/h IAS.
 
Takeoff speed: 180..200 km/h
Glideslope speed: 195..205 km/h
Landing speed: 135..145 km/h
Landing angle: 15 °
 
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 and turn times are given for Boosted power.
 
Engine:
Model: AM-35a
Maximum power in Boosted mode at sea level: 1350 HP
Maximum power in Nominal mode at sea level: 1120 HP
Maximum power in Nominal mode at 6000 m: 1200 HP
 
Engine modes:
Nominal (unlimited time): 2050 RPM, 1040 mm Hg
Boosted power (up to 10 minutes): 2050 RPM, 1240 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: 2650 kg
Minimum weight (no ammo, 10% fuel): 2831 kg
Standard weight: 3244 kg
Maximum takeoff weight: 3476 kg
Fuel load: 352 kg / 480 l
Useful load: 826 kg
 
Forward-firing armament:
2 x 7.62mm machine gun "ShKAS", 750 rounds, 1800 rounds per minute, synchronized
12.7mm machine gun "UB", 300 rounds, 1000 rounds per minute, synchronized
2 x 12.7mm machine gun "UB", 145 rounds, 1000 rounds per minute, wing-mounted (modification)
2 x 12.7mm machine gun "UB", 350 rounds, 1000 rounds per minute, synchronized (modification)
2 x 20mm gun "SsVAK", 150 rounds, 800 rounds per minute, synchronized (modification)
 
Bombs:
2 x 50 kg general purpose bombs "FAB-50sv"
2 x 104 kg general purpose bombs "FAB-100M"
 
Rockets:
6 x 7 kg rockets "ROS-82", HE payload mass 2.52 kg
 
Length: 8.255 m
Wingspan: 10.2 m
Wing surface: 17.44 m²
 
Combat debut: July 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 shutters are controlled manually.
- The aircraft has only pitch and yaw flight-control trimmers.
- The aircraft has automatic wing slats. They deploy when the high angle of attack increases which makes pre-stall softer.
- Landing flaps have a limiter for the maximum angle. The flaps have an extended range from 0° to 50°. The landing flaps have pneumatic actuator. Flaps can only be instantly extended to the angle which is set by limiter, gradual extending is impossible. Due to weak force of the actuator the extended landing flaps may retract upward by the airflow when the airspeed is more than 220 km/h. For this reason, it is necessary to remember that 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 right before landing.
- The aircraft has a tailwheel control system which is unlocked and made controllable by the rudder if the rudder pedal is pressed more than for 40% of its range. The tailwheel remans locked if pedals are deflected less than 40%. Because of this, it is necessary to avoid large rudder pedal inputs when moving at high speed, or be ready to control the airplane with an unlocked tailwheel should large rudder inputs be made.
- 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 total remaining fuel.
- It is impossible to open or close the canopy at high speed due to strong airflow. The canopy has no emergency release, so bail out requires the speed drop before it.
- When bombs are installed there is a salvo controller, it has two release modes: single drop or drop two in a salvo.
- When rockets are installed there is a salvo controller, it has three launch modes: single fire, fire two in a salvo or fire four in a salvo.
 
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/cowl flap control handle: close
- 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
 
3.1 Recommended positions of the oil radiator control handle for various flight modes:
- takeoff: open 100%
- climb: open 100% (winter: 50%)
- cruise flight: open 50% (winter: 20%)
- combat: close
 
3.2 Recommended positions of the water radiator control handle for various flight modes:
- takeoff: open 100% (winter: 25%)
- climb: open 100% (winter: 25%)
- cruise flight: open 40% (winter: 20%)
- combat: open 100%
 
4. Approximate fuel consumption at 2000 m altitude:
- Cruise engine mode: 6.0 l/min
- Combat engine mode: 7.2 l/min
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