MC.202 Series VIII

**MC.202 Series VIII** is an Italian fighter available as part of *Battle of Moscow* (Collector's Edition).

## Specifications

```
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 m^2

Combat debut: June 1942

```

### Additional Configurations

```
Breda SAFAT 7.7mm wing-mounted machineguns with 500 rounds per each
Additional mass: 49 kg
Ammunition mass: 24 kg
Guns mass: 25 kg
Estimated speed loss: 0 km/h

MG 151/20 20mm guns in wing-mounted gun pods with 135 rounds per each
Additional mass: 212 kg
Ammunition mass: 55 kg
Guns mass: 157 kg
Estimated speed loss: 15 km/h

2 x 55 kg General Purpose Bombs 50-T
Additional mass: 130 kg
Ammunition mass: 110 kg
Racks mass: 20 kg
Estimated speed loss before drop: 14 km/h
Estimated speed loss after drop: 7 km/h

100 kg General Purpose Bomb 100-T
Additional mass: 220 kg
Ammunition mass: 200 kg
Racks mass: 20 kg
Estimated speed loss before drop: 20 km/h
Estimated speed loss after drop: 7 km/h

Additional pilot protection: armoured triplex wind screen
Additional mass: 10 kg
Estimated speed loss: 0 km/h

```