il2

MC.202 ser.VIII

Description

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%25 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 tail wheel 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.

Modifications

2 x 7.7mm machineguns
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

2 x 50-T bombs
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

2 x 20mm MG 151/20 gun pods
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

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

2 x 100-T bombs
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