IL-2 AM-38 (model 1941)

The IL-2 AM-38 (model 1941) is a Russian attack aircraft available in Battle of Moscow.

Specifications
 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 m^2

Combat debut: June 1941

Additional Configurations
 2 VYa-23 23mm wing-mounted guns with 150 rounds per each Additional mass: 110 kg Ammunition mass: 170 kg Guns mass: 132 kg Estimated speed loss: 1 km/h

6 x 50 kg General Purpose Bombs FAB-50sv / 6 x 104 kg General Purpose Bombs FAB-100M FAB-50sv: Additional mass: 300 kg Ammunition mass: 300 kg Estimated speed loss before drop: 5 km/h Estimated speed loss after drop: 0 km/h FAB-100M: Additional mass: 624 kg Ammunition mass: 624 kg Estimated speed loss before drop: 9 km/h Estimated speed loss after drop: 0 km/h

2 x 254 kg General Purpose Bombs FAB-250sv Additional mass: 538 kg Ammunition mass: 508 kg Racks mass: 30 kg Estimated speed loss before drop: 19 km/h Estimated speed loss after drop: 9 km/h

8 x 82mm Armour Piercing unguided rockets RBS-82 Additional mass: 144 kg Ammunition mass: 120 kg Racks mass: 24 kg Estimated speed loss before launch: 13 km/h Estimated speed loss after launch: 8 km/h

8 x 132mm High Explosive unguided rockets ROFS-132 Additional mass: 376 kg Ammunition mass: 336 kg Racks mass: 40 kg Estimated speed loss before launch: 20 km/h Estimated speed loss after launch: 12 km/h