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This content needs the base game IL-2 Sturmovik: Battle of Stalingrad along Aerosol in order to play.

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Composes 5 items: IL-2 Sturmovik: Battle of The seat of power, IL-2 Sturmovik: 10 counts Timespan of Autumn Campaign, IL-2 Sturmovik: P-40E-1 Collector Military aircraft, IL-2 Sturmovik: MC.202 Collector Plane, IL-2 Sturmovik: Battle of Stalingrad

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About The situation Content

Fly the Italian Macchi 202, no optimal Italian fighter plane that saw action at which Eastern front of WWII!In the match, she has the option to launch Macchi 202 throughout Career style during Battle in respect to The seat of power and Battle of Stalingrad timeframes, in multiplayer and in Quick Mission Builder.The Macchi combines rather moderate scale of German Messerschmitts with the robustness of a Focke-Wulf. It incorporates unique tough framework with all-metal construction throughout the airframe and two-spar wings, the only anomalous case being the rudder. A unique signature of the Macchi is its peculiar wing design which is is asymmetrical. The left aile turns 20 cm longer in lieu of the right one to counteract torque produced by the engine. An wings don’t have leading edge slats and the landing gear is generally similar to the FW-190 which is quite wide likewise serviceable. There’s each trim stabilizer for the elevators, as opposed to nay trim segments on any distinct flight surface.The ultimately stance in the direction of the composition design is certain bit surprising: on the one member the aircraft is aerodynamically clean and well designed; on the other hand both of its radiator cowlings look ill-placed causing much drag. The engine is an export version of the DB601A that was also used in earlier Bf-109 schemes. But as against the Bf-109s in our game, this one doesn’t have an good automated constant-speed propeller mechanism. The Macchi’s propeller only has couple fundamental settings: 2200 and 2400 angular velocity. All another systems are expand to the pilot to set up and prolong by controlling the prop pitch manually. Water and biofuel radiator controls are reference material as well. Keep amid memory that Macchi’s throttle relocation is also inverted – forward to slow retreating and back to accelerate.

• Armament: 2 x 12.7mm Breda SAFAT gear guns with 400 stages and per rate of fire of 700 rounds per minute.
• Length: 8.85 m (29.03 ft.)
• Wingspan: 10.58 mature (34.7 ft.)
• Wing envelope: 16.8 sq. m (55.11 sq. ft.)

Modifications

• Additional aircraft operator security: armored triplex windscreen (10 kg / 22 lbs. weight increase)
• 2 x additional Breda SAFAT 7.7mm wing-mounted automaton guns with 500 stints per gun. (25 - 49 kg / 55 – 108 lbs. encumbrance increase)
• 2 x additional MG 151/20 20mm guns in wing-mounted blaster pods with 135 trials per gun (157 - 212 kg / 346 – 467 lbs. weight increase, 15 kph / 24 mph speed loss)
• 2 x 50-T General Purpose Bombs (130 kg / 287 lbs. significance increase with nuke racks, 14 kph / 9 velocity speed loss, 7 kph / 4 mph speed loss after drop)
• 2 x 100-T General Purpose Torpedoes (220 kg / 485 metric tons. weight increase with bomb cases, 20 kph / 12 mph speed loss, 7 kph / 4 mph speed deterioration due to drop)

Skins

• Standard shape with winter camo
• 2./JG 108, ('214' besides Luftwaffe markings used along training unit)
• 73°Squadriglia, 9°Gruppo, 4°Stormo C.T., Tenente Giulio Reiner, Fuka, Egypt, July 1942 ('73-7' dark seafoam green accompanied by sand blotches and light grey bottom)
• 386a°Squadriglia, 21°Gruppo Autonomo C.T., Kantemirowka, USSR, October 1942 ('386-1' light sienna with dark green segments and light grey undersides)
• 70°Squadriglia, 23°Gruppo, 3°Stormo C.T., Cerveteri, Italy, August 1943 ('2-70' flash cinnamon coupled with demanding pitch-black basil patches and light grey undersides)
• 71°a Squadriglia, 17°Gruppo, 1°Stormo C.T., Udine-Campoformido, Italy, October 1941 ('71-2' cryptic olive green and light grey undersides)
• 369°a Squadriglia, 22°Gruppo, 53°Stormo C.T., Capodichino, Italy, Summer 1943 ('369-12' light tawny in the presence of dark lime rings and light grey undersides)
• 378°a Squadriglia, 155°Gruppo, 51°Stormo C.T., Gela, Italy, August 1943 ('378-4' overcast green with yellow and brown shards and light grey undersides)
• Aeromacchi C.202 prototype introductory flown upon Lonate Pozollo on August 10, 1940 by chief test pilot Guido Carestiato (metal with no pigment with a handful of branches painted with protective primer color)
• 2./Jagd Lehrer Überprüfungsgruppe, Konrad Augner ('13' light brown with midnight green patches, light grey undersides and yellow markings)

Flight Parameters

Indicated stall speed along run configuration: 151..166 km/hIndicated stall zest in takeoff/landing configuration: 139..152 km/hDive speed limit: 850 km/hMaximum payload factor: 14.8 GStall angle of attack in flight configuration: 19.6 °Stall angle of attack in landing structure: 17.4 °Maximum true air speed at sea level, engine mode - Confrontation: 500 km/hMaximum true air speed outside 2000 m, drivetrain mode - War: 543 km/hMaximum true air speed at 5000 main, engine mode - War against: 604 km/hService ceiling: 11300 mClimb rate near sea level: 17.3 m/sClimb rate at 3000 m: 15.1 m/sClimb rate adjacent to 6000 m: 10.6 m/sMaximum performance turn at sea stage: 22.6 s, at 270 km/h IAS.Maximum performance alter under 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/hGlideslope hastiness: 190..200 km/hLanding zest: 140..150 km/hLanding angle: 13.9 °Note 1: both inputs distributed is for international policy atmosphere (ISA).Note 2: flight performance ranges are given in exchange for possible aircraft mass ranges.Note 3: unlimited speeds, climb rates as well turn times are given on behalf of standard aircraft mass.Note 4: climb tariffs are given for Confrontation power, turn times are due to for Boosted power.Engine:Model: RA.1000Maximum stamina in Boosted design at sea level: 1175 HPMaximum power in Combat mode at sea level: 1050 HPMaximum mastery in Combat method at 3700 m: 1100 HPEngine modes:Nominal (unlimited time): 2200 RPM, 1.23 ataCombat power (up after 5 minutes): 2400 RPM, 1.35 ataBoosted power (up to 1 minute): 2500 RPM, 1.45 ataWater rated temperature along motor unit intake: 70..80 °CWater rated temperature in engine output: 94 °CWater maximum temperature in engine output: 100 °COil examined temperature within the bounds of engine intake: 60..75 °COil utmost extent temperature in engine intake: 85 °COil benchmarked temperature by engine output: 90..100 °COil maximum temperature beneath engine output: 110 °CSupercharger materials shift altitude: pliant coupling Empty bulk: 2448 kgMinimum weight (no ammo, 10%25 fuel): 2622 kgStandard weight: 2967 kgMaximum propulsion weight: 3197 kgFuel load: 307 kilogram / 430 lUseful load: 749 kgCombat rollout: Sunshine days 1942

Operation features

• Throttle lever is inverted: backward = full throttle, forward = idle throttle.
• Engine is equipped with automatic mixture control system on top of supercharger with fluid coupling which does not require manual control.
• Engine RPM has an automatic chancellor with a pair of fixed modes: 2200 SHAFT SPEED normal mode, 2400 TURNOVER RATE boosted mode. At the same time, it is possible to turn off some other governor and control the propeller pitch manually over mechanical actuator.
• Water and condensate radiator shutters are controlled manually.
• Airplane has no flight-control trimmers. Airplane is equipped with bendable trim tabs that can be set pre-flight by base personnel.
• Airplane has asymmetric half-wings relating to roll-compensation: the left representative is 20 cm longer than right one.
• Airplane has that via human effort regulated horizontal stabilizer. It should be set to dispassionate up to takeoff and disembarkation. Also, it may be used to trim the flight stick during the flight. In a deep fall the stabilizer should remain set so when either pilot must push the flight stick forward to maintain the sink into angle.
• Landing flaps have a hydraulic actuator and they can be extended to any angle up to 45°. The flap system comprehends a "pneumatic spring" which allows flaps to be pressed upwards by airflow at airspeed more than 200 km/h.
• Airplane has a manual stem axle lock. Wheel be obliged to be jammed when taxiing straight with respect to random considerable displacement and before takeoff and landing.
• Airplane commands discrepancy pneumatic wheel brakes with the shared control lever. This means that if the brake lever is arranged and its rudder pedal the opposite circular disk brake feels gradually released eliciting the zeppelin to swing after one side or the other.
• Airplane has a fuel gauge which indicates only the front fuel tank level.
• The design of the cockpit canopy does not allow it to be swung during runway. The canopy should be closed before takeoff to prevent damage. The canopy has an emergency release system for bailouts.
• The govern system for the bomb rack only allows to drop bombs one by one.
• The gunsight displays a sliding sun-filter. There is also a back-up folding mechanical sight which can be used if main sight comprises damaged.

System Requirements

Minimum:
• Requires a 64-bit processor and operating system
• OS: 64-bit Windows® 10/11
• Processor: Intel® Core™ i5/i7 3+ GHz
• Memory: 16 GB RAM
• Graphics: 4GB VRAM or better
• DirectX: Version 11
• Storage: 85 GB available space
• VR Comfort: SteamVR. Keyboard and mouse required
• Additional Notes: DirectX®-compatible flight stick recommended

Recommended:
• Requires a 64-bit processor and operating system

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