IL-2 AM-38 modèle 1941: Questions / Réponses
Publié : dim. janv. 31, 2016 11:05 pm
Le but de ce topic est de rassembler toute les infos concernant cette appareils afin de facilité les recherches et la prise en main.N'hésitez pas à apporter vos connaissances.
Caractéristique dans le jeu:
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 °
Ground speed at sea level, engine mode - Boosted: 430 km/h
Ground speed at sea level, engine mode - Nominal (at 2150 RPM): 421 km/h
Maximum ground 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
Standart 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
Unlock of additional airplane configuration:
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
Unlock of additional airplane configuration:
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
Unlock of additional airplane configuration:
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
Unlock of additional airplane configuration:
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
Unlock of additional airplane configuration:
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
Il-2 (Model 1941):
Plane is fitted with an oxygen system
Oil and water radiators can be controlled via analog or keyboard commands.
Adjustable Trim: pitch
Tail Wheel: lockable
One control panel governs the release of both bombs and rockets, as well as one trigger on the flight stick. There is a switchboard to the right of the pilot that will move up & down when firing/releasing bombs or rockets and when setting their release mode. All keyboard commands for bombs and rockets are the same as before.
Vidéo de familiarisation par Requiem:
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