MC.202 ser.VIII / IL-2 Sturmovik: Great Battles
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Fighter
MC.202 ser.VIII
History
Specifications

The experience of combat operations in Spain led both the Italian and the Soviet command to the conclusion that it was necessary to rearm their air forces with more modern fighter models. In 1939, the Fiat CR.42 "Falco," Fiat G.50 "Freccia," and Macchi C.200 "Saetta" fighters, powered by the Fiat A.74 RC.38 air-cooled engine, went into production. However, the first air battles with the latest French and British fighters showed that these machines were inferior to their opponents in all characteristics: one of the reasons was a weak engine with high drag, and Italy did not yet produce water-cooled aircraft engines. Therefore, at the beginning of 1940, the "McKee" company bought a copy of the German Daimler-Benz DB 601 in-line engine, which had already been successfully used in the Bf 109 fighter. The company's chief designer Mario Castoldi and a group of engineers proactively developed a new fighter, designated M.C.202. The aircraft was developed based on the M.C.200 fighter, which was characterized by good controllability and manufacturability.

The M.C.202 "Folgore" ("Lightning") was an all-metal fighter-interceptor. The newly designed compact fuselage was aerodynamically clean. The solid construction of the fuselage and wings had smooth rivets on all surfaces and careful "sanding" of all surfaces. The power of the liquid-cooled Daimler-Benz DB 601 engine, produced under license by Alfa Romeo under the designation R.A.1000 RC41, was 1175 hp (1100 hp in combat mode at an altitude of 3700 m). The cooling of the engine was well thought out and included, besides water cooling with several water pumps, additional air intakes to supply air to the cylinder heads. The fighter had a closed cockpit canopy that opened to the side and a short upper rear dorsal spine that served as a headrest and roll cage. A unique feature of the aircraft was the asymmetric wing: to compensate for engine torque, the left wingtip was 21 cm longer than the right.

The aircraft of the VIII series differed from the first ones in terms of armament: in addition to two large-caliber machine guns in the nose of the fuselage, two more machine guns of rifle caliber were installed in the wings, starting with the VI series.

In 1942, 50 Series VIII aircraft were built, which began arriving at the front in June.

The "Folgore" was the first truly world-class fighter for the Royal Italian Air Force. Its excellent aerodynamics, high speed, and maneuverability, combined with excellent climb rate and pilot comfort, placed it among the best fighters of the early period of World War II. The M.C.202 saw action in Africa and in the skies over Malta, Sicily, and Italy.

In September 1942, 12 M.C.202s were sent to the USSR to replenish the Royal Italian Air Force units on the Eastern Front. They were part of the 21st Fighter Group, which was mainly armed with M.C.200s. The aircraft were evenly distributed among the squadrons. These units participated in the offensive of the Italian 8th Army towards the Don and in the defense of Stalingrad. The M.C.202s fought Soviet Yak and LaGG fighters and supported their troops with ground attack missions. Between August 1941 and January 1943 the M.C.200 and 202 flew a total of 6,361 sorties to gain air superiority, support troops and attack ground targets.

Sources used:

1. Gianni Cattaneo "The Macchi C.202" Aircraft Profile, 28 1965

2. "С. Kedrov "Macchi" - avid warriors (Italian fighters of Mario Castoldi)" Journal "Wings of the Motherland" 6 1999.

3. Materials of the site airwar.ru

Indicated stall speed in flight configuration: 151..166 km/h
Indicated stall speed in takeoff/landing configuration: 139..152 km/h
Dive speed limit: 850 km/h
Maximum load factor: 14.8 G
Stall angle of attack in flight configuration: 19.6 °
Stall angle of attack in landing configuration: 17.4 °
 
Maximum true air speed at sea level, engine mode - Combat: 500 km/h
Maximum true air speed at 2000 m, engine mode - Combat: 543 km/h
Maximum true air speed at 5000 m, engine mode - Combat: 604 km/h
 
Service ceiling: 11300 m
Climb rate at sea level: 17.3 m/s
Climb rate at 3000 m: 15.1 m/s
Climb rate at 6000 m: 10.6 m/s
 
Maximum performance turn at sea level: 22.6 s, at 270 km/h IAS.
Maximum performance turn at 3000 m: 28.2 s, at 270 km/h IAS.
 
Flight endurance at 3000 m: 2.2 h, at 350 km/h IAS.
 
Takeoff speed: 160..190 km/h
Glideslope speed: 190..200 km/h
Landing speed: 140..150 km/h
Landing angle: 13.9 °
 
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 Boosted power.
 
Engine:
Model: RA.1000
Maximum power in Boosted mode at sea level: 1175 HP
Maximum power in Combat mode at sea level: 1050 HP
Maximum power in Combat mode at 3700 m: 1100 HP
 
Engine modes:
Nominal (unlimited time): 2200 RPM, 1.23 ata
Combat power (up to 5 minutes): 2400 RPM, 1.35 ata
Boosted power (up to 1 minute): 2500 RPM, 1.45 ata
 
Water rated temperature in engine intake: 70..80 °C
Water rated temperature in engine output: 94 °C
Water maximum temperature in engine output: 100 °C
Oil rated temperature in engine intake: 60..75 °C
Oil maximum temperature in engine intake: 85 °C
Oil rated temperature in engine output: 90..100 °C
Oil maximum temperature in engine output: 110 °C
 
Supercharger gear shift altitude: fluid coupling 
 
Empty weight: 2448 kg
Minimum weight (no ammo, 10% fuel): 2622 kg
Standard weight: 2967 kg
Maximum takeoff weight: 3197 kg
Fuel load: 307 kg / 430 l
Useful load: 749 kg
 
Forward-firing armament:
2 x 12.7mm machine gun "Breda SAFAT 12.7", 400 rounds, 700 rounds per minute, synchronized
2 x 7.7mm machine gun "Breda SAFAT 7.7", 500 rounds, 900 rounds per minute, wing-mounted (modification)
2 x 20mm gun "MG 151/20", 135 rounds, 700 rounds per minute, wing-mounted (modification)
 
Bombs:
2 x 50 kg general purpose bombs "50-T"
2 x 100 kg general purpose bombs "100-T"
 
Length: 8.85 m
Wingspan: 10.58 m
Wing surface: 16.8 m²
 
Combat debut: June 1942
 
Operation features:
- Throttle lever is inverted: backward = full throttle, forward = idle throttle.
- The engine is equipped with automatic mixture control system and supercharger with fluid coupling which does not require manual control.
- Engine RPM has an automatic governor with two fixed modes: 2200 RPM normal mode, 2400 RPM boosted mode. Also, it is possible to turn off the governor and control the propeller pitch manually by mechanical actuator.
- Water and oil radiator shutters are controlled manually.
- 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 asymmetric half-wings for roll-compensation: the left one is 20 cm longer than right one.
- The aircraft has a manually controlled horizontal stabilizer. It should be set to neutral 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.
- Landing flaps have a hydraulic actuator and they can be extended to any angle up to 45°. The flap system includes a "pneumatic spring" which allows flaps to be pressed upwards by airflow at airspeed more than 200 km/h.
- 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 indicates only the front fuel tank level.
- The design of the cockpit canopy does not allow it to be opened during flight. The canopy should be closed before takeoff to prevent damage. The canopy has an emergency release system for bailouts.
- The control system for the bomb rack only allows to drop bombs one by one.
- The gunsight has a sliding sun-filter. There is also a back-up folding mechanical sight which can be used if main sight is damaged.
 
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 oil/water radiator control handle: close
- recommended position of the prop pitch control handle: light
- recommended position of the throttle lever: 0%
- before taxiing, you must unlock the tailwheel
 
2. Recommended mixture control lever positions for various flight modes: auto mixture control
 
3.1 Recommended positions of the oil radiators control handle for various flight modes:
- takeoff: open 100%
- climb: open 100%
- cruise flight: open 100% (in winter conditions - open 50%)
- combat: open 50%
 
3.2 Recommended positions of the water radiators control handle for various flight modes:
- takeoff: open 100%
- climb: open 100%
- cruise flight: open 100% (in winter conditions - close if necessary)
- combat: open 50%
 
4. Approximate fuel consumption at 2000 m altitude:
- Cruise engine mode: 5.7 l/min
- Combat engine mode: 6.8 l/min
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