IL-2 Sturmovik Flugzeuginformationen - LW

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IL-2 Sturmovik Flugzeuginformationen - LW

Beitrag von I/JG27_Zimmi » Di 27 Dez 2016, 18:10

Originalbeitrag: https://forum.il2sturmovik.com/topic/25 ... erational/



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Indicated stall speed in flight configuration: 152..159 km/h
Indicated stall speed in takeoff/landing configuration: 147..146 km/h
Dive speed limit: 850 km/h
Maximum load factor: 11 G
Stall angle of attack in flight configuration: 20 °
Stall angle of attack in landing configuration: 16.6 °

Maximum true air speed at sea level, engine mode - Emergency: 477 km/h
Maximum true air speed at 2000 m, engine mode - Emergency: 520 km/h
Maximum true air speed at 5000 m, engine mode - Emergency: 564 km/h

Service ceiling: 10500 m
Climb rate at sea level: 14 m/s
Climb rate at 3000 m: 13.3 m/s
Climb rate at 6000 m: 7 m/s

Maximum performance turn at sea level: 20.5 s, at 270 km/h IAS.
Maximum performance turn at 3000 m: 25.5 s, at 270 km/h IAS.

Flight endurance at 3000 m: 2.2 h, at 350 km/h IAS.

Takeoff speed: 140..170 km/h
Glideslope speed: 180..190 km/h
Landing speed: 130..140 km/h
Landing angle: 14.3 °

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: DB-601A
Maximum power in Boosted mode at sea level: 1100 HP
Maximum power in Emergency mode at sea level: 990 HP
Maximum power in Emergency mode at 4500 m: 1020 HP
Maximum power in Combat mode at sea level: 910 HP
Maximum power in Combat mode at 5000 m: 960 HP

Engine modes:
Nominal (unlimited time): 2200 RPM, 1.15 ata
Combat power (up to 30 minutes): 2300 RPM, 1.23 ata
Emergency power (up to 5 minutes): 2400 RPM, 1.3 ata
Boosted power (up to 1 minute): 2400 RPM, 1.4 ata

Water rated temperature in engine output: 94 °C
Water maximum temperature in engine output: 100 °C
Oil rated temperature in engine intake: 30..75 °C
Oil maximum temperature in engine intake: 80 °C
Oil rated temperature in engine output: 95 °C
Oil maximum temperature in engine output: 105 °C

Supercharger gear shift altitude: fluid coupling

Empty weight: 2049 kg
Minimum weight (no ammo, 10% fuel): 2340 kg
Standard weight: 2614 kg
Maximum takeoff weight: 2893 kg
Fuel load: 304 kg / 400 l
Useful load: 844 kg

Forward-firing armament:
2 x 20mm gun "MG FF", 60 rounds, 540 rounds per minute, wing-mounted
2 x 7.92mm machine gun "MG 17", 1000 rounds, 1200 rounds per minute, synchronized

Bombs:

Up to 4 x 55 kg general purpose bombs "SC 50"
249 kg general purpose bomb "SC 250"

Length: 8.8 m
Wingspan: 9.9 m
Wing surface: 16.4 m^2

Combat debut: August 1940

Additional airplane configurations list:

4 x 55 kg General Purpose Bombs SC 50
Additional mass: 260 kg
Ammunition mass: 220 kg
Racks mass: 40 kg
Estimated speed loss before drop: 53 km/h
Estimated speed loss after drop: 13 km/h

249 kg General Purpose Bomb SC 250
Additional mass: 279 kg
Ammunition mass: 249 kg
Racks mass: 30 kg
Estimated speed loss before drop: 34 km/h
Estimated speed loss after drop: 11 km/h

Removed pilot armoured headrest for improved field of view
Weight savings: 8 kg
Estimated speed loss: 0 km/h

Additional pilot protection: armoured triplex wind screen
Additional mass: 20 kg
Estimated speed loss: 1 km/h

Additional protection: armoured plates on bottom of plane
Additional mass: 89 kg
Estimated speed loss: 4 km/h

Operation features:
- Airplane has a wide automatization of the engine systems, in fact, to control speed it is only necessary to use the throttle lever. There is no need to manually set engine revolutions and mixture or supercharger gear in normal flight.
- To reduce swinging during taxiing due to prop-wash the propeller pitch control should be switched to manual mode and pitch should be reduced to minimum.
- Water and oil 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 ground personnel.
- Airplane has a manually controlled horizontal stabilizer. It should be set to +1° before takeoff and to -4°...-5° before 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.
- Airplane has automatic wing slats. They deploy when the high angle of attack increases which makes pre-stall softer.
- Airplane has a manual mechanical system for retracting the landing flaps, for this reason it is necessary to extend landing flaps well before final approach. Markers on the left-wing flap indicate how far the flaps are extended. The flaps can be extended to any angle up to 42°.
- Airplane has a manual tail wheel lock. Wheel should be locked when taxiing straight for a long distance and before takeoff and landing.
- Airplane has independent left and right hydraulic wheel brake controls. To apply either brake push the upper part of the rudder pedal.
- Airplane has a fuel gauge which shows total fuel remaining. Also, it has an emergency fuel warning light (80 liters).
- 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 for dropping bombs one by one.
- The gunsight has a sliding sun-filter.
OLt. Zimmermann
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Re: IL-2 Sturmovik Flugzeuginformationen - LW

Beitrag von I/JG27_Zimmi » Di 27 Dez 2016, 18:22

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Indicated stall speed in flight configuration: 151..168 km/h
Indicated stall speed in takeoff/landing configuration: 144 km/h..159 km/h
Dive speed limit: 850 km/h
Maximum load factor: 11 G
Stall angle of attack in flight configuration: 19.7 °
Stall angle of attack in landing configuration: 17 °

Maximum true air speed at sea level, engine mode - Emergency: 528 km/h
Maximum true air speed at 2000 m, engine mode - Emergency: 563 km/h
Maximum true air speed at 5000 m, engine mode - Emergency: 606 km/h

Service ceiling: 11500 m
Climb rate at sea level: 16.4 m/s
Climb rate at 3000 m: 14.1 m/s
Climb rate at 6000 m: 10 m/s

Maximum performance turn at sea level: 23.6 s, at 270 km/h IAS.
Maximum performance turn at 3000 m: 29.0 s, at 270 km/h IAS.

Flight endurance at 3000 m: 2.4 h, at 350 km/h IAS.

Takeoff speed: 145..175 km/h
Glideslope speed: 185..195 km/h
Landing speed: 135..145 km/h
Landing angle: 14.8 °

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: DB-601N
Maximum power in Boosted mode at 5500 m: 1220 HP
Maximum power in Emergency mode at sea level: 1175 HP
Maximum power in Emergency mode at 4900 m: 1175 HP
Maximum power in Combat mode at sea level: 1015 HP
Maximum power in Combat mode at 4900 m: 1045 HP

Engine modes:
Nominal (unlimited time): 2300 RPM, 1.15 ata
Combat power (up to 30 minutes): 2400 RPM, 1.25 ata
Emergency power (up to 3 minutes): 2600 RPM, 1.35 ata
Boosted power (up to 1 minute): 2800 RPM, 1.42 ata

Water rated temperature in engine output: 100..102 °C
Water maximum temperature in engine output: 110 °C
Oil rated temperature in engine intake: 70..80 °C
Oil maximum temperature in engine intake: 85 °C

Supercharger gear shift altitude: fluid coupling

Empty weight: 2171 kg
Minimum weight (no ammo, 10% fuel): 2445 kg
Standard weight: 2789 kg
Maximum takeoff weight: 3092 kg
Fuel load: 304 kg / 400 l
Useful load: 921 kg

Forward-firing armament:
15mm gun "MG 151/15", 200 rounds, 700 rounds per minute, nose-mounted
2 x 7.92mm machine gun "MG 17", 500 rounds, 1200 rounds per minute, synchronized
20mm gun "MG 151/20", 200 rounds, 700 rounds per minute, nose-mounted (modification)

Bombs:
Up to 4 x 55 kg general purpose bombs "SC 50"
249 kg general purpose bomb "SC 250"

Length: 8.94 m
Wingspan: 9.97 m
Wing surface: 16.1 m^2

Combat debut: March 1941

Additional airplane configurations list:

MG 151/20 20mm nose-gun with 200 rounds
Additional mass: 4 kg
Ammunition mass: 42 kg
Gun mass: 44 kg
Estimated speed loss: 0 km/h

4 x 55 kg General Purpose Bombs SC 50
Additional mass: 260 kg
Ammunition mass: 220 kg
Racks mass: 40 kg
Estimated speed loss before drop: 51 km/h
Estimated speed loss after drop: 11 km/h

249 kg General Purpose Bomb SC 250
Additional mass: 279 kg
Ammunition mass: 249 kg
Racks mass: 30 kg
Estimated speed loss before drop: 31 km/h
Estimated speed loss after drop: 10 km/h

Removed pilot armoured headrest for improved field of view
Weight savings: 8 kg
Estimated speed loss: 0 km/h

Additional pilot protection: armoured triplex wind screen
Additional mass: 20 kg
Estimated speed loss: 1 km/h

Operation features:
- Airplane has a wide automatization of the engine systems, in fact, to control speed it is only necessary to use the throttle lever. There is no need to manually set engine revolutions and mixture or supercharger gear in normal flight.
- In addition to full-automatic mode there is a special emergency mode for the radiator shutters, which can be used in specific situations. In this mode, the shutters are forced to be fully opened.
- To reduce swinging during taxiing due to prop-wash the propeller pitch control should be switched to manual mode and pitch should be reduced to minimum.
- Airplane has no flight-control trimmers. Airplane is equipped with bendable trim tabs that can be set pre-flight by ground personnel.
- Airplane has a manually controlled horizontal stabilizer. It should be set to +1° before takeoff and to -4°...-5° before 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.
- Airplane has automatic wing slats. They deploy when the high angle of attack increases which makes pre-stall softer.
- Airplane has a manual mechanical system for retracting the landing flaps, for this reason it is necessary to extend landing flaps well before final approach. Markers on the left-wing flap indicate how far the flaps are extended. The flaps can be extended to any angle up to 40°.
- Airplane has a manual tail wheel lock. Wheel should be locked when taxiing straight for a long distance and before takeoff and landing.
- Airplane has independent left and right hydraulic wheel brake controls. To apply either brake push the upper part of the rudder pedal.
- Airplane has a fuel gauge which shows total fuel remaining. Also, it has an emergency fuel warning light (80 liters).
- 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 for dropping bombs one by one.
- The gunsight has a sliding sun-filter.
OLt. Zimmermann
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Re: IL-2 Sturmovik Flugzeuginformationen - LW

Beitrag von I/JG27_Zimmi » Di 27 Dez 2016, 18:34

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Indicated stall speed in flight configuration: 148..182 km/h
Indicated stall speed in takeoff/landing configuration: 131..162 km/h
Dive speed limit: 740 km/h
Maximum load factor: 11 G
Stall angle of attack in flight configuration: 20.7 °
Stall angle of attack in landing configuration: 17.5 °

Maximum true air speed at sea level, engine mode - Emergency: 456 km/h
Maximum true air speed at 2000 m, engine mode - Emergency: 494 km/h
Maximum true air speed at 5000 m, engine mode - Emergency: 529 km/h

Service ceiling: 9500 m
Climb rate at sea level: 10.3 m/s
Climb rate at 3000 m: 9.6 m/s
Climb rate at 6000 m: 6.1 m/s

Maximum performance turn at sea level: 27.4 s, at 270 km/h IAS.
Maximum performance turn at 3000 m: 35.4 s, at 270 km/h IAS.

Flight endurance at 3000 m: 3.5 h, at 300 km/h IAS.

Takeoff speed: 180..220 km/h
Glideslope speed: 200..220 km/h
Landing speed: 140..160 km/h
Landing angle: 10.6 °

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: DB-601A
Maximum power in Boosted mode at sea level: 1100 HP
Maximum power in Emergency mode at sea level: 990 HP
Maximum power in Emergency mode at 4500 m: 1020 HP
Maximum power in Combat mode at sea level: 910 HP
Maximum power in Combat mode at 5000 m: 960 HP

Engine modes:
Nominal (unlimited time): 2200 RPM, 1.15 ata
Combat power (up to 30 minutes): 2300 RPM, 1.23 ata
Emergency power (up to 5 minutes): 2400 RPM, 1.3 ata
Boosted power (up to 1 minute): 2400 RPM, 1.4 ata

Water rated temperature in engine output: 94 °C
Water maximum temperature in engine output: 100 °C
Oil rated temperature in engine intake: 30..75 °C
Oil maximum temperature in engine intake: 80 °C
Oil rated temperature in engine output: 95 °C
Oil maximum temperature in engine output: 105 °C

Supercharger gear shift altitude: fluid coupling

Empty weight: 5175 kg
Minimum weight (no ammo, 10% fuel): 5597 kg
Standart weight: 6706 kg
Maximum takeoff weight: 8398 kg
Fuel load: 965 kg / 1270 l
Useful load: 3223 kg

Forward-firing armament:
4 x 7.92mm machine gun "MG 17", 1000 rounds, 1200 rounds per minute, nose-mounted
2 x 20mm gun "MG FF", 180 rounds, 540 rounds per minute, nose-mounted

Defensive armament:
Backward: 7.92mm machine gun "MG 15", 825 rounds, 1000 rounds per minute

Bombs:
Up to 12 x 55 kg general purpose bombs "SC 50"
Up to 2 x 249 kg general purpose bombs "SC 250"
Up to 2 x 500 kg general purpose bombs "SC 500"
1090 kg general purpose bomb "SC 1000"

Length: 12.1 m
Wingspan: 16.3 m
Wing surface: 38.4 m^2

Combat debut: October 1940

Additional airplane configurations list:

12 x 55 kg General Purpose Bombs SC 50
Additional mass: 820 kg
Ammunition mass: 660 kg
Racks mass: 160 kg
Estimated speed loss before drop: 80 km/h
Estimated speed loss after drop: 38 km/h

2 x 500 kg General Purpose Bomb SC 500
Additional mass: 1025 kg
Ammunition mass: 1000 kg
Racks mass: 50 kg
Estimated speed loss before drop: 35 km/h
Estimated speed loss after drop: 5 km/h

1090 kg General Purpose Bomb SC 1000
Additional mass: 1140 kg
Ammunition mass: 1090 kg
Racks mass: 50 kg
Estimated speed loss before drop: 33 km/h
Estimated speed loss after drop: 5 km/h

Additional pilot protection: armoured triplex wind screen and armoured headrest
Additional mass: 32 kg
Estimated speed loss: 0 km/h

Additional protection: armoured plates on engines and radiators
Additional mass: 245 kg
Estimated speed loss: 0 km/h

Operation features:
- Airplane has a wide automatization of the engine systems, in fact, to control speed it is only necessary to use the throttle lever. There is no need to manually set engine revolutions and mixture or supercharger gear in normal flight.
- Water and oil radiator shutters are controlled manually. The oil radiator control has five fixed positions. The water radiator control has nine fixed positions.
- Propellers have a feathering system which should be activated in case of engine damage to reduce drag of the propeller in auto-rotation.
- To reduce swinging during taxiing due to prop-wash it is necessary to use asymmetrical engines thrust. It is recommended to give the left engine 20% more power. Also, the propeller pitch control should be switched to manual mode and pitch should be reduced to minimum.
- Airplane has only pitch and yaw flight-control trimmers.
- Airplane has automatic wing slats. They deploy when the high angle of attack increases which makes pre-stall softer.
- Landing flaps have a hydraulic actuator and they can be extended to any angle up to 50°.
- Airplane has a automatically controlled horizontal stabilizer. An automatic control system adjusts the stabilizer angle depending on the extended angle of the landing flaps.
- Airplane tail wheel rotates freely and does not have a lock. For this reason, it is necessary to confidently and accurately operate the rudder pedals during the takeoff and landing.
- Airplane has independent left and right hydraulic wheel brake controls. To apply either brake push the upper part of the rudder pedal.
- Airplane has a fuel gauge which shows the reaming fuel in one of four fuel tanks depending on the switch position. In the game the fuel indicator switch changes by itself during horizontal flight by every 10 seconds. Also, the airplane has a low fuel warning light (50 liters) for each tank.
- 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.
- Airplane is equipped with an automatic bomb salvo controller, it allows you to choose which bomb-racks to be released (central belly, left and right wing) and to switch the bomb salvo (single release or release all bombs).
- Reloading of both MG-FF guns (forward and rearward) must be performed by the rear gunner. The forward firing MGFF must be reloaded at the pilot's command.
- The gunsight has a sliding sun-filter.
OLt. Zimmermann
Gruppenkommandeur

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Re: IL-2 Sturmovik Flugzeuginformationen - LW

Beitrag von I/JG27_Zimmi » Di 27 Dez 2016, 18:49


Bild

Indicated stall speed in flight configuration: 188..205 km/h
Indicated stall speed in takeoff/landing configuration: 158..185 km/h
Dive speed limit: 670 km/h
Maximum load factor: 8.0 G
Stall angle of attack in flight configuration: 21.0 °
Stall angle of attack in landing configuration: 16.6 °

Maximum true air speed at sea level, engine mode - Climb: 424 km/h
Maximum true air speed at 2000 m, engine mode - Climb: 462 km/h
Maximum true air speed at 5000 m, engine mode - Climb: 486 km/h

Service ceiling: 7500 m
Climb rate at sea level: 7.0 m/s
Climb rate at 3000 m: 5.1 m/s
Climb rate at 6000 m: 3.4 m/s

Maximum performance turn at sea level: 33.0 s, at 250 km/h IAS.
Maximum performance turn at 3000 m: 50.5 s, at 250 km/h IAS.

Flight endurance at 3000 m: 3.8 h, at 300 km/h IAS.

Takeoff speed: 170..210 km/h
Glideslope speed: 210..220 km/h
Landing speed: 150..160 km/h
Landing angle: 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 Climb power, turn times are given for Take-off power.

Engine:
Model: Jumo-211J
Maximum power in Take-off mode at sea level: 1420 HP
Maximum power in Climb mode at sea level: 1190 HP
Maximum power in Climb mode at 1500 m: 1260 HP
Maximum power in Climb mode at 4900 m: 1180 HP

Engine modes:
Nominal (unlimited time): 2250 RPM, 1.15 ata
Climb power (up to 30 minutes): 2400 RPM, 1.25 ata
Take-off power (up to 1 minute): 2600 RPM, 1.42 ata

Water rated temperature in engine output: 80 °C
Water maximum temperature in engine output: 110 °C
Oil rated temperature in engine output: 100 °C
Oil maximum temperature in engine output: 130 °C

Supercharger gear shift altitude: automatic

Empty weight: 8619 kg
Minimum weight (no ammo, 10% fuel): 9458 kg
Standard weight: 12110 kg
Maximum takeoff weight: 13655 kg
Fuel load: 1277 kg / 1680 l
Useful load: 5036 kg

Defensive armament:
Nose: 7.92mm machine gun "MG 81", 750 rounds, 1600 rounds per minute
Top: 7.92mm machine gun "MG 81", 1000 rounds, 1600 rounds per minute
Belly: 2 x 7.92mm machine gun "MG 81", 950 rounds, 1600 rounds per minute

Bombs:
Up to 44 x 55 kg general purpose bombs "SC 50"
Up to 6 x 249 kg general purpose bombs "SC 250"
Up to 4 x 500 kg general purpose bombs "SC 500"
Up to 2 x 1090 kg general purpose bombs "SC 1000"
1780 kg general purpose bomb "SC 1800"

Length: 14.3 m
Wingspan: 20.02 m
Wing surface: 52.7 m^2

Combat debut: June 1941

Additional airplane configurations list:

44 x 55 kg General Purpose Bombs SC 50
Additional mass: 2640 kg
Ammunition mass: 2420 kg
Racks mass: 220 kg
Estimated speed loss before drop: 97 km/h
Estimated speed loss after drop: 39 km/h

6 x 249 kg General Purpose Bomb SC 250 (+2 on the underwing holders)
Additional mass: 1544 kg
Ammunition mass: 1494 kg
Racks mass: 50 kg
Estimated speed loss before drop: 37 km/h
Estimated speed loss after drop: 4 km/h

4 x 500 kg General Purpose Bomb SC 500
Additional mass: 2000 kg
Ammunition mass: 2000 kg
Estimated speed loss before drop: 34 km/h
Estimated speed loss after drop: 0 km/h

2 x 1090 kg General Purpose Bomb SC 1000
Additional mass: 2180 kg
Ammunition mass: 2180 kg
Estimated speed loss before drop: 26 km/h
Estimated speed loss after drop: 0 km/h

1780 kg General Purpose Bomb SC 1800
Additional mass: 1780 kg
Ammunition mass: 1780 kg
Estimated speed loss before drop: 23 km/h
Estimated speed loss after drop: 0 km/h

Operation features:
- Each engine has a two-stage mechanical supercharger with an automatic switch system that switches gears depending altitude and engine revolutions. It can also be manually switched to first gear.
- Engine mixture control is automatic.
- Engine RPM has an automatic governor and it is maintained at the required RPM corresponding to the governor control lever position. The governor automatically controls the propeller pitch to maintain the required RPM.
- Propellers have a feathering system which should be activated in case of engine damage to reduce drag of the propeller in auto-rotation.
- Water and oil radiators shutters are joint with engine cowl outlet shutters and manually operated. Ground personnel may install additional fixed shutters on the intake of the oil radiators in cold weather to prevent freezing of the oil
- Airplane has trimmers for all flight-controls: pitch, roll, yaw.
- Airplane has fence-type airbrakes which are located under the wing and used to slow the descent during steep dive bombing.
- Airplane has hydraulic-actuated landing flaps with three fixed positions: retracted, takeoff (25°) and landing (50°). Flap indicator lights are located on left panel.
- Airplane has a automatically controlled horizontal stabilizer. An automatic control system adjusts the stabilizer angle depending on the extended angle of the landing flaps. The stabilizer control lamps are located near the flaps indicator lights.
- Airplane is also equipped with differential ailerons which are lowered in synch with the flaps.
- Lowering the landing gear takes a long time, for this reason it is necessary to extend the landing gear well before final landing approach.
- Airplane tail wheel rotates freely and does not have a lock. For this reason, it is necessary to confidently and accurately operate the rudder pedals during the takeoff and landing.
- Airplane has independent left and right hydraulic wheel brake controls. To apply either brake push the upper part of the rudder pedal.
- Airplane has dedicated fuel gauges for left and right fuel tank groups and there is a switch between the internal and external fuel tank group indicator. In game the fuel indicator switch changes by itself during horizontal flight every 10 seconds. Also, the airplane has low fuel warning lights (180 liters) for the internal tanks.
- Airplane is equipped with an automatic bomb salvo controller, it allows the pilot to switch between the bomb racks to be released (internal or external) and to switch between different salvo quantities. There is also a controller for a drop delay between each bomb in the salvo.
OLt. Zimmermann
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Re: IL-2 Sturmovik Flugzeuginformationen - LW

Beitrag von I/JG27_Zimmi » Di 27 Dez 2016, 18:51


Bild

Indicated stall speed in flight configuration: 154..171 km/h
Indicated stall speed in takeoff/landing configuration: 148..161 km/h
Dive speed limit: 850 km/h
Maximum load factor: 11 G
Stall angle of attack in flight configuration: 19.9 °
Stall angle of attack in landing configuration: 17 °

Maximum true air speed at sea level, engine mode - Combat: 522 km/h
Maximum true air speed at 2000 m, engine mode - Combat: 570 km/h
Maximum true air speed at 6000 m, engine mode - Combat: 635 km/h

Service ceiling: 11600 m
Climb rate at sea level: 19.5 m/s
Climb rate at 3000 m: 18.8 m/s
Climb rate at 6000 m: 14.9 m/s

Maximum performance turn at sea level: 20.3 s, at 270 km/h IAS.
Maximum performance turn at 3000 m: 26.1 s, at 270 km/h IAS.

Flight endurance at 3000 m: 2.6 h, at 350 km/h IAS.

Takeoff speed: 150..180 km/h
Glideslope speed: 190..200 km/h
Landing speed: 145..155 km/h
Landing angle: 14.8 °

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 Emergency power.

Engine:
Model: DB-601E
Maximum power in Emergency mode at sea level: 1350 HP
Maximum power in Emergency mode at 4800 m: 1320 HP
Maximum power in Combat mode at sea level: 1200 HP
Maximum power in Combat mode at 4900 m: 1200 HP

Engine modes:
Nominal (unlimited time): 2300 RPM, 1.15 ata
Combat power (up to 30 minutes): 2500 RPM, 1.3 ata
Emergency power (up to 1 minute): 2700 RPM, 1.42 ata

Water rated temperature in engine output: 100..102 °C
Water maximum temperature in engine output: 115 °C
Oil rated temperature in engine intake: 70..80 °C
Oil maximum temperature in engine intake: 85 °C

Supercharger gear shift altitude: fluid coupling

Empty weight: 2382 kg
Minimum weight (no ammo, 10% fuel): 2545 kg
Standard weight: 2890 kg
Maximum takeoff weight: 3189 kg
Fuel load: 304 kg / 400 l
Useful load: 807 kg

Forward-firing armament:
20mm gun "MG 151/20", 200 rounds, 700 rounds per minute, nose-mounted
2 x 7.92mm machine gun "MG 17", 500 rounds, 1200 rounds per minute, synchronized
2 x 15mm gun "MG 151/15", 135 rounds, 700 rounds per minute, wing-mounted (modification)
2 x 20mm gun "MG 151/20", 135 rounds, 700 rounds per minute, wing-mounted (modification)

Bombs:
Up to 4 x 55 kg general purpose bombs "SC 50"
249 kg general purpose bomb "SC 250"

Length: 8.94 m
Wingspan: 9.97 m
Wing surface: 16.1 m^2

Combat debut: June 1941

Additional airplane configurations list:

MG 151/15 15mm guns in wing-mounted gun pods with 135 rounds per each
Additional mass: 193 kg
Ammunition mass: 47 kg
Guns mass: 146 kg
Estimated speed loss: 11 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: 12 km/h

4 x 55 kg General Purpose Bombs SC 50
Additional mass: 260 kg
Ammunition mass: 220 kg
Racks mass: 40 kg
Estimated speed loss before drop: 51 km/h
Estimated speed loss after drop: 11 km/h

249 kg General Purpose Bomb SC 250
Additional mass: 279 kg
Ammunition mass: 249 kg
Racks mass: 30 kg
Estimated speed loss before drop: 31 km/h
Estimated speed loss after drop: 10 km/h

Removed pilot armoured headrest for improved field of view
Weight savings: 8 kg
Estimated speed loss: 0 km/h

Additional pilot protection: armoured triplex wind screen
Additional mass: 20 kg
Estimated speed loss: 1 km/h

Operation features:
- Airplane has a wide automatization of the engine systems, in fact, to control speed it is only necessary to use the throttle lever. There is no need to manually set engine revolutions and mixture or supercharger gear in normal flight.
- In addition to full-automatic mode there is a special manual control mode for the radiator shutters, which can be used in specific situations.
- To reduce swinging during taxiing due to prop-wash the propeller pitch control should be switched to manual mode and pitch should be reduced to minimum.
- Airplane has no flight-control trimmers. Airplane is equipped with bendable trim tabs that can be set pre-flight by ground personnel.
- Airplane has a manually controlled horizontal stabilizer. It should be set to +1° before takeoff and to -4°...-5° before 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.
- Airplane has automatic wing slats. They deploy when the high angle of attack increases which makes pre-stall softer.
- Airplane has a manual mechanical system for retracting the landing flaps, for this reason it is necessary to extend landing flaps well before final approach. Markers on the left-wing flap indicate how far the flaps are extended. The flaps can be extended to any angle up to 40°.
- Airplane has a manual tail wheel lock. Wheel should be locked when taxiing straight for a long distance and before takeoff and landing.
- Airplane has independent left and right hydraulic wheel brake controls. To apply either brake push the upper part of the rudder pedal.
- Airplane has a fuel gauge which shows total fuel remaining. Also, it has an emergency fuel warning light (80 liters).
- 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 for dropping bombs one by one.
- The gunsight has a sliding sun-filter.
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Re: IL-2 Sturmovik Flugzeuginformationen - LW

Beitrag von I/JG27_Zimmi » Di 27 Dez 2016, 18:53

Bild

Indicated stall speed in flight configuration: 158..174 km/h
Indicated stall speed in takeoff/landing configuration: 153..164 km/h
Dive speed limit: 850 km/h
Maximum load factor: 10.5 G
Stall angle of attack in flight configuration: 19.8 °
Stall angle of attack in landing configuration: 17 °

Maximum true air speed at sea level, engine mode - Combat: 525 km/h
Maximum true air speed at 2000 m, engine mode - Combat: 569 km/h
Maximum true air speed at 7000 m, engine mode - Combat: 648 km/h

Service ceiling: 12100 m
Climb rate at sea level: 22.3 m/s
Climb rate at 3000 m: 19.6 m/s
Climb rate at 6000 m: 16.0 m/s

Maximum performance turn at sea level: 22.2 s, at 270 km/h IAS.
Maximum performance turn at 3000 m: 28.3 s, at 270 km/h IAS.

Flight endurance at 3000 m: 2.4 h, at 350 km/h IAS.

Takeoff speed: 155..180 km/h
Glideslope speed: 195..205 km/h
Landing speed: 150..155 km/h
Landing angle: 14.8 °

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 and turn times are given for Combat power.

Engine:
Model: DB-605A
Maximum power in Combat mode at sea level: 1310 HP
Maximum power in Combat mode at 5800 m: 1250 HP

Engine modes:
Nominal (unlimited time): 2300 RPM, 1.15 ata
Combat power (up to 30 minutes): 2600 RPM, 1.3 ata

Water rated temperature in engine output: 100..102 °C
Water maximum temperature in engine output: 115 °C
Oil rated temperature in engine intake: 70..80 °C
Oil maximum temperature in engine intake: 85 °C

Supercharger gear shift altitude: fluid coupling

Empty weight: 2486 kg
Minimum weight (no ammo, 10% fuel): 2649 kg
Standard weight: 2994 kg
Maximum takeoff weight: 3283 kg
Fuel load: 304 kg / 400 l
Useful load: 797 kg

Forward-firing armament:
20mm gun "MG 151/20", 200 rounds, 700 rounds per minute, nose-mounted
2 x 7.92mm machine gun "MG 17", 500 rounds, 1200 rounds per minute, synchronized
2 x 20mm gun "MG 151/20", 135 rounds, 700 rounds per minute, wing-mounted (modification)

Bombs:
Up to 4 x 55 kg general purpose bombs "SC 50"
249 kg general purpose bomb "SC 250"

Length: 8.94 m
Wingspan: 9.97 m
Wing surface: 16.1 m^2

Combat debut: May 1942

Additional airplane configurations list:

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: 12 km/h

4 x 55 kg General Purpose Bombs SC 50
Additional mass: 260 kg
Ammunition mass: 220 kg
Racks mass: 40 kg
Estimated speed loss before drop: 51 km/h
Estimated speed loss after drop: 11 km/h

249 kg General Purpose Bomb SC 250
Additional mass: 279 kg
Ammunition mass: 249 kg
Racks mass: 30 kg
Estimated speed loss before drop: 31 km/h
Estimated speed loss after drop: 10 km/h

Alternative pilot protection: armoured transparent triplex head rest for better visibility
Additional mass: 10 kg
Estimated speed loss: 0 km/h

Removed pilot armoured headrest for improved field of view
Weight savings: 8 kg
Estimated speed loss: 0 km/h

Operation features:
- Airplane has a wide automatization of the engine systems, in fact, to control speed it is only necessary to use the throttle lever. There is no need to manually set engine revolutions and mixture or supercharger gear in normal flight.
- In addition to full-automatic mode there is a special manual control mode for the radiator shutters, which can be used in specific situations.
- To reduce swinging during taxiing due to prop-wash the propeller pitch control should be switched to manual mode and pitch should be reduced to minimum.
- Airplane has no flight-control trimmers. Airplane is equipped with bendable trim tabs that can be set pre-flight by ground personnel.
- Airplane has a manually controlled horizontal stabilizer. It should be set to +1° before takeoff and to -4°...-5° before 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.
- Airplane has automatic wing slats. They deploy when the high angle of attack increases which makes pre-stall softer.
- Airplane has a manual mechanical system for retracting the landing flaps, for this reason it is necessary to extend landing flaps well before final approach. Markers on the left-wing flap indicate how far the flaps are extended. The flaps can be extended to any angle up to 40°.
- Airplane has a manual tail wheel lock. Wheel should be locked when taxiing straight for a long distance and before takeoff and landing.
- Airplane has independent left and right hydraulic wheel brake controls. To apply either brake push the upper part of the rudder pedal.
- Airplane has a fuel gauge which shows total fuel remaining. Also, it has an emergency fuel warning light (80 liters).
- 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 for dropping bombs one by one.
- The gunsight has a sliding sun-filter.
OLt. Zimmermann
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Re: IL-2 Sturmovik Flugzeuginformationen - LW

Beitrag von I/JG27_Zimmi » Di 27 Dez 2016, 18:58


Bild

Indicated stall speed in flight configuration: 137..176 km/h
Indicated stall speed in takeoff/landing configuration: 123..155 km/h

Dive speed limit: 650 km/h
Maximum load factor: 9 G
Stall angle of attack in flight configuration: 19.9 °
Stall angle of attack in landing configuration: 18 °

Maximum true air speed at sea level, engine mode - Climb: 367 km/h
Maximum true air speed at 2000 m, engine mode - Climb: 389 km/h
Maximum true air speed at 6000 m, engine mode - Climb: 422 km/h

Service ceiling: 7000 m
Climb rate at sea level: 8 m/s
Climb rate at 3000 m: 7 m/s
Climb rate at 6000 m: 2.5 m/s

Maximum performance turn at sea level: 22.2 s, at 230 km/h IAS.
Maximum performance turn at 3000 m: 31.3 s, at 230 km/h IAS.

Flight endurance at 3000 m: 3.4 h, at 300 km/h IAS.

Takeoff speed: 140..170 km/h
Glideslope speed: 180..195 km/h
Landing speed: 125..145 km/h
Landing angle: 11 °

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 Climb power, turn times are given for Take-off power.

Engine:
Model: Jumo-211J
Maximum power in Take-off mode at sea level: 1420 HP
Maximum power in Climb mode at sea level: 1190 HP
Maximum power in Climb mode at 1500 m: 1260 HP
Maximum power in Climb mode at 4900 m: 1180 HP

Engine modes:
Nominal (unlimited time): 2250 RPM, 1.15 ata
Climb power (up to 30 minutes): 2400 RPM, 1.25 ata
Take-off power (up to 1 minute): 2600 RPM, 1.42 ata

Water rated temperature in engine output: 80 °C
Water maximum temperature in engine output: 110 °C
Oil rated temperature in engine output: 90 °C
Oil maximum temperature in engine output: 105 °C

Supercharger gear shift altitude: automatic

Empty weight: 3930 kg
Minimum weight (no ammo, 10% fuel): 4250 kg
Standard weight: 4835 kg
Maximum takeoff weight: 6684 kg
Fuel load: 626 kg / 840 l
Useful load: 2754 kg

Forward-firing armament:
2 x 7.92mm machine gun "MG 17", 1000 rounds, 1200 rounds per minute, nose-mounted
12 x 7.92mm machine gun "MG 81", 250 rounds, 1600 rounds per minute, wing-mounted (modification)
2 x 37mm gun "BK 37", 12 rounds, 160 rounds per minute, wing-mounted (modification)

Defensive armament:
Backward: 2 x 7.92mm machine gun "MG 81", 500 rounds, 1600 rounds per minute

Bombs:
Up to 4 x 70 kg general purpose bomb "SD 70"
Up to 3 x 249 kg general purpose bombs "SC 250"
500 kg general purpose bomb "SC 500"
1090 kg general purpose bomb "SC 1000"
1780 kg general purpose bomb "SC 1800"

Length: 11 m
Wingspan: 13.8 m
Wing surface: 31.9 m^2

Combat debut: March 1942

Additional airplane configurations list:

2 gun pods with 3 twin 7.92mm MG-81Z machineguns and 1500 rounds per each pod
Additional mass: 369 kg
Ammunition mass: 89 kg
Guns mass: 280 kg
Estimated speed loss: 31 km/h

2 gun pods with 37mm autocannons 3.7cm BK with 12 rounds per each
Additional mass: 793 kg
Ammunition mass: 31 kg
Guns mass: 840 kg
Estimated speed loss: 33 km/h

1780 kg General Purpose Bomb SC 1800
Additional mass: 1780 kg
Ammunition mass: 1780 kg
Estimated speed loss before drop: 28 km/h
Estimated speed loss after drop: 0 km/h

Special impeller-actuated siren for demoralizing enemies in dive attacks
Additional mass: 9 kg
Estimated speed loss: 12 km/h

Additional pilot protection: armoured plates on side of cockpit and canopy
Additional mass: 60 kg
Estimated speed loss: 0 km/h

Operation features:
- The engine has a two-stage mechanical supercharger with an automatic switch system that switches gears depending altitude and engine revolutions. It can also be manually switched to first gear.
- Engine mixture control is automatic.
- Engine RPM has an automatic governor and it is maintained at the required RPM corresponding to the governor control lever position. The governor automatically controls the propeller pitch to maintain the required RPM.
- Water and oil radiators shutters control is manual.
- Airplane has only the pitch and roll flight-control trimmers.
- Airplane has fence-type airbrakes which are located under the wing and used to slow the descent during steep dive bombing.
- Airplane has hydraulic-actuated landing flaps with three fixed positions: retracted, takeoff (25°) and landing (40°). Flap indicator lights are located on left panel near the throttle.
- Airplane is also equipped with differential ailerons which are lowered in synch with the flaps.
- Airplane has a automatically controlled horizontal stabilizer. An automatic control system adjusts the stabilizer angle depending on the extended angle of the landing flaps. The stabilizer control lamps are located near the throttle lever.
- Airplane has a manual tail wheel lock. Wheel should be locked when taxiing straight for a long distance and before takeoff and landing.
- Airplane has independent left and right hydraulic wheel brake controls. To apply either brake push the upper part of the rudder pedal.
- Airplane have a fuel gauge which shows remaining fuel in left and right fuel tanks depending on switch position. In game the fuel indicator switch changes by itself during horizontal flight by every 10 seconds. Also, the airplane has indicator lights for full internal tanks and a low fuel warning light (160 liters) for each tank.
- It is impossible to open or close canopy at high speed due to strong airflow. When the canopy is open, it is impossible to use rear gun because it is linked to canopy. The canopy has an emergency release system for bailouts.
- Airplane has a window in the cockpit floor which can be opened by the bomb bay door command.
- Airplane is equipped with a salvo controller, it allows the pilot to choose which bomb racks to use (central, left and right wing) and to switch the bomb salvo (single drop or all bombs on the rack).
- The gunsight has a sliding sun-filter.
OLt. Zimmermann
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Re: IL-2 Sturmovik Flugzeuginformationen - LW

Beitrag von I/JG27_Zimmi » Di 27 Dez 2016, 19:00


Bild

Indicated stall speed in flight configuration: 150..184 km/h
Indicated stall speed in takeoff/landing configuration: 123..151 km/h
Dive speed limit: 560 km/h
Maximum load factor: 4.5 G
Stall angle of attack in flight configuration: 20 °
Stall angle of attack in landing configuration: 17 °

Maximum true air speed at sea level, engine mode - Climb: 369 km/h
Maximum true air speed at 2000 m, engine mode - Climb: 398 km/h
Maximum true air speed at 5000 m, engine mode - Climb: 405 km/h

Service ceiling: 6300 m
Climb rate at sea level: 4.5 m/s
Climb rate at 3000 m: 3.6 m/s
Climb rate at 6000 m: 1.8 m/s

Maximum performance turn at sea level: 30.8 s, at 250 km/h IAS.
Maximum performance turn at 3000 m: 45.2 s, at 250 km/h IAS.

Flight endurance at 3000 m: 8.5 h, at 300 km/h IAS.

Takeoff speed: 170..210 km/h
Glideslope speed: 180..200 km/h
Landing speed: 125..150 km/h
Landing angle: 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 Climb power, turn times are given for Take-off power.

Engine:
Model: Jumo-211J
Maximum power in Take-off mode at sea level: 1420 HP
Maximum power in Climb mode at sea level: 1190 HP
Maximum power in Climb mode at 1500 m: 1260 HP
Maximum power in Climb mode at 4900 m: 1180 HP

Engine modes:
Nominal (unlimited time): 2250 RPM, 1.15 ata
Climb power (up to 30 minutes): 2400 RPM, 1.25 ata
Take-off power (up to 1 minute): 2600 RPM, 1.42 ata

Water rated temperature in engine output: 80 °C
Water maximum temperature in engine output: 110 °C
Oil rated temperature in engine output: 90 °C
Oil maximum temperature in engine output: 105 °C

Supercharger gear shift altitude: automatic

Empty weight: 8963 kg
Minimum weight (no ammo, 10% fuel): 9946 kg
Standard weight: 13727 kg
Maximum takeoff weight: 15239 kg
Fuel load: 3214 kg / 4285 l
Useful load: 6276 kg

Defensive armament:
Nose: 7.92mm machine gun "MG 15", 600 rounds, 1000 rounds per minute
Top: 7.92mm machine gun "MG 15", 1125 rounds, 1000 rounds per minute
Belly-backward: 7.92mm machine gun "MG 15", 1200 rounds, 1000 rounds per minute
Belly-forward: 7.92mm machine gun "MG 15", 675 rounds, 1000 rounds per minute
Left: 7.92mm machine gun "MG 15", 450 rounds, 1000 rounds per minute
Right: 7.92mm machine gun "MG 15", 450 rounds, 1000 rounds per minute
Nose: 20mm gun "MG FF", 240 rounds, 540 rounds per minute (modification)
Belly-forward: 20mm gun "MG FF", 330 rounds, 540 rounds per minute (modification)

Bombs:
Up to 16 x 55 kg general purpose bombs "SC 50"
Up to 4 x 249 kg general purpose bombs "SC 250"
500 kg general purpose bomb "SC 500"
Up to 2 x 1090 kg general purpose bombs "SC 1000"
Up to 2 x 1780 kg general purpose bombs "SC 1800"
2400 kg general purpose bomb "SC 2500"

Length: 16.38 m
Wingspan: 22.5 m
Wing surface: 79.5 m^2

Combat debut: June 1941

Additional airplane configurations list:

2 x 1090 kg General Purpose Bomb SC 1000
Additional mass: 2180 kg
Ammunition mass: 2180 kg
Estimated speed loss before drop: 23 km/h
Estimated speed loss after drop: 0 km/h

2 x 1780 kg General Purpose Bomb SC 1800
Additional mass: 3560 kg
Ammunition mass: 3560 kg
Estimated speed loss before drop: 32 km/h
Estimated speed loss after drop: 0 km/h

2400 kg General Purpose Bomb SC 2500
Additional mass: 2400 kg
Ammunition mass: 2400 kg
Estimated speed loss before drop: 17 km/h
Estimated speed loss after drop: 0 km/h

Nose turret with 20mm MG FF gun with 240 rounds
Additional mass: 46 kg
Estimated speed loss: 0 km/h

Belly forward-looking turret with 20mm MG FF gun with 300 rounds
Additional mass: 147 kg
Estimated speed loss: 0 km/h

Operation features:
- Each engine has a two-stage mechanical supercharger with an automatic switch system that switches gears depending altitude and engine revolutions. It can also be manually switched to first gear.
- Engine mixture control is automatic.
- Engine RPM has an automatic governor and it is maintained at the required RPM corresponding to the governor control lever position. The governor automatically controls the propeller pitch to maintain the required RPM.
- Propellers have a feathering system which should be activated in case of engine damage to reduce drag of the propeller in auto-rotation.
- Water and oil radiator shutter controls are manual. The oil radiator control has five fixed positions.
- Airplane has trimmers for all flight-controls: pitch, roll and yaw.
- Landing flaps have a hydraulic actuator and they can be extended to any angle up to 60°.
- Airplane tail wheel rotates freely and does not have a lock. For this reason, it is necessary to confidently and accurately operate the rudder pedals during the takeoff and landing.
- Airplane has independent left and right hydraulic wheel brake controls. To apply either brake push the upper part of the rudder pedal.
- Airplane has dedicated fuel gauges for left and right fuel tank groups and there is a switch between the internal and external fuel tank group indicator. In game the fuel indicator switch changes by itself during horizontal flight every 10 seconds. Also, there is dedicated fuel gauge for the fuselage fuel tank. Also, the airplane has low fuel warning lights (200 liters) for left and right fuel tank groups.
- Airplane is equipped with an automatic bomb salvo controller, it allows you to switch between the bomb racks to be released (internal or external) and to switch between different salvo quantities. There is also a controller for a drop delay between each bomb in the salvo.
OLt. Zimmermann
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Re: IL-2 Sturmovik Flugzeuginformationen - LW

Beitrag von I/JG27_Zimmi » Di 27 Dez 2016, 19:06

Bild

Indicated stall speed in flight configuration: 165..175 km/h
Indicated stall speed in takeoff/landing configuration: 154..167 km/h
Dive speed limit: 850 km/h
Maximum load factor: 10.5 G
Stall angle of attack in flight configuration: 19.8 °
Stall angle of attack in landing configuration: 17 °

Maximum true air speed at sea level, engine mode - Emergency: 540 km/h
Maximum true air speed at sea level, engine mode - Combat: 517 km/h
Maximum true air speed at 2000 m, engine mode - Combat: 564 km/h
Maximum true air speed at 7000 m, engine mode - Combat: 640 km/h

Service ceiling: 11800 m
Climb rate at sea level: 20.1 m/s
Climb rate at 3000 m: 18.9 m/s
Climb rate at 6000 m: 15.4 m/s

Maximum performance turn at sea level: 21.2 s, at 270 km/h IAS.
Maximum performance turn at 3000 m: 27.2 s, at 270 km/h IAS.

Flight endurance at 3000 m: 2.4 h, at 350 km/h IAS.

Takeoff speed: 155..180 km/h
Glideslope speed: 195..205 km/h
Landing speed: 150..155 km/h
Landing angle: 13.7 °

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 and turn times are given for Combat power.

Engine:
Model: DB-605A
Maximum power in Emergency mode at sea level: 1480 HP
Maximum power in Emergency mode at 5600 m: 1360 HP
Maximum power in Combat mode at sea level: 1310 HP
Maximum power in Combat mode at 5800 m: 1250 HP

Engine modes:
Nominal (unlimited time): 2300 RPM, 1.15 ata
Combat power (up to 30 minutes): 2600 RPM, 1.3 ata
Emergency power (up to 1 minute): 2800 RPM, 1.42 ata

Water rated temperature in engine output: 100..102 °C
Water maximum temperature in engine output: 115 °C
Oil rated temperature in engine intake: 70..80 °C
Oil maximum temperature in engine intake: 85 °C

Supercharger gear shift altitude: fluid coupling

Empty weight: 2506 kg
Minimum weight (no ammo, 10% fuel): 2669 kg
Standard weight: 3014 kg
Maximum takeoff weight: 3303 kg
Fuel load: 304 kg / 400 l
Useful load: 797 kg

Forward-firing armament:
20mm gun "MG 151/20", 200 rounds, 700 rounds per minute, nose-mounted
2 x 7.92mm machine gun "MG 17", 500 rounds, 1200 rounds per minute, synchronized
2 x 20mm gun "MG 151/20", 135 rounds, 700 rounds per minute, wing-mounted (modification)

Bombs:
Up to 4 x 55 kg general purpose bombs "SC 50"
249 kg general purpose bomb "SC 250"

Length: 8.94 m
Wingspan: 9.97 m
Wing surface: 16.1 m^2

Combat debut: spring 1943

Additional airplane configurations list:

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: 12 km/h

4 x 55 kg General Purpose Bombs SC 50
Additional mass: 260 kg
Ammunition mass: 220 kg
Racks mass: 40 kg
Estimated speed loss before drop: 51 km/h
Estimated speed loss after drop: 11 km/h

249 kg General Purpose Bomb SC 250
Additional mass: 279 kg
Ammunition mass: 249 kg
Racks mass: 30 kg
Estimated speed loss before drop: 31 km/h
Estimated speed loss after drop: 10 km/h

Alternative pilot protection: armoured transparent triplex head rest for better visibility
Additional mass: 10 kg
Estimated speed loss: 0 km/h

Removed pilot armoured headrest for improved field of view
Weight savings: 8 kg
Estimated speed loss: 0 km/h

Operation features:
- Airplane has a wide automatization of the engine systems, in fact, to control speed it is only necessary to use the throttle lever. There is no need to manually set engine revolutions and mixture or supercharger gear in normal flight.
- In addition to full-automatic mode there is a special manual control mode for the radiator shutters, which can be used in specific situations.
- To reduce swinging during taxiing due to prop-wash the propeller pitch control should be switched to manual mode and pitch should be reduced to minimum.
- Airplane has no flight-control trimmers. Airplane is equipped with bendable trim tabs that can be set pre-flight by ground personnel.
- Airplane has a manually controlled horizontal stabilizer. It should be set to +1° before takeoff and to -4°...-5° before 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.
- Airplane has automatic wing slats. They deploy when the high angle of attack increases which makes pre-stall softer.
- Airplane has a manual mechanical system for retracting the landing flaps, for this reason it is necessary to extend landing flaps well before final approach. Markers on the left-wing flap indicate how far the flaps are extended. The flaps can be extended to any angle up to 40°.
- Airplane has a manual tail wheel lock. Wheel should be locked when taxiing straight for a long distance and before takeoff and landing.
- Airplane has independent left and right hydraulic wheel brake controls. To apply either brake push the upper part of the rudder pedal.
- Airplane has a fuel gauge which shows total fuel remaining. Also, it has an emergency fuel warning light (80 liters).
- 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.
OLt. Zimmermann
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Re: IL-2 Sturmovik Flugzeuginformationen - LW

Beitrag von I/JG27_Zimmi » Di 27 Dez 2016, 19:07

Bild

Indicated stall speed in flight configuration: 183..209 km/h
Indicated stall speed in takeoff/landing configuration: 167..190 km/h
Dive speed limit: 850 km/h
Maximum load factor: 11 G
Stall angle of attack in flight configuration: 15.5°
Stall angle of attack in landing configuration: 14.1°

Maximum true air speed at sea level, engine mode - Emergency: 555 km/h
Maximum true air speed at 3000 m, engine mode - Emergency: 574 km/h
Maximum true air speed at 6700 m, engine mode - Emergency: 667 km/h

Service ceiling: 10800 m
Climb rate at sea level: 16.4 m/s
Climb rate at 3000 m: 12.4 m/s
Climb rate at 6000 m: 10.1 m/s

Maximum performance turn at sea level: 24.7 s, at 280 km/h IAS.
Maximum performance turn at 3000 m: 34.3 s, at 270 km/h IAS.

Flight endurance at 3000 m: 3.2 h, at 350 km/h IAS.

Takeoff speed: 170..210 km/h
Glideslope speed: 205..215 km/h
Landing speed: 160..170 km/h
Landing angle: 12.5°

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 Emergency power.

Engine:
Model: BMW-801D
Maximum power in Emergency mode at sea level: 1700 HP
Maximum power in Emergency mode at 5700 m: 1440 HP
Maximum power in Combat mode at 700 m: 1520 HP
Maximum power in Combat mode at 5300 m: 1320 HP

Engine modes:
Nominal (unlimited time): 2300 RPM, 1.2 ata
Combat power (up to 30 minutes): 2400 RPM, 1.32 ata
Emergency power (up to 3 minutes): 2700 RPM, 1.42 ata

Oil rated temperature in engine intake: 60..70 °C
Oil maximum temperature in engine intake: 85 °C
Oil rated temperature in engine output: 105 °C
Oil maximum temperature in engine output: 120 °C
Cylinder head rated temperature: 180 °C
Cylinder head maximum temperature: 220 °C
Supercharger gear shift altitude: automatic

Empty weight: 3148 kg
Minimum weight (no ammo, 10% fuel): 3330 kg
Standard weight: 3855 kg
Maximum takeoff weight: 4385 kg
Fuel load: 409 kg / 524 l
Useful load: 1237 kg

Forward-firing armament:
2 x 20mm gun "MG 151/20", 250 rounds, 700 rounds per minute, synchronized
2 x 7.92mm machine gun "MG 17", 900 rounds, 1200 rounds per minute, synchronized
2 x 20mm gun "MG FF", 90 rounds, 540 rounds per minute, wing-mounted (modification)

Bombs:
Up to 4 x 55 kg general purpose bombs "SC 50"
249 kg general purpose bomb "SC 250"
500 kg general purpose bomb "SC 500"

Length: 8.85 m
Wingspan: 10.51 m
Wing surface: 18.3 m^2

Combat debut: March 1942

Additional airplane configurations list:

MG FF/M 20mm additional wing-mounted guns with 60 rounds per each
Additional mass: 123 kg
Ammunition mass: 29 kg
Guns mass: 94 kg
Estimated speed loss: 7 km/h

MG FF/M 20mm additional wing-mounted guns with 90 rounds per each
Additional mass: 144 kg
Ammunition mass: 50 kg
Guns mass: 94 kg
Estimated speed loss: 8 km/h

4 x 55 kg General Purpose Bombs SC 50
Additional mass: 280 kg
Ammunition mass: 220 kg
Racks mass: 60 kg
Estimated speed loss before drop: 85 km/h
Estimated speed loss after drop: 41 km/h

249 kg General Purpose Bomb SC 250
Additional mass: 279 kg
Ammunition mass: 249 kg
Racks mass: 30 kg
Estimated speed loss before drop: 37 km/h
Estimated speed loss after drop: 11 km/h

500 kg General Purpose Bomb SC 500
Additional mass: 530 kg
Ammunition mass: 500 kg
Racks mass: 30 kg
Estimated speed loss before drop: 43 km/h
Estimated speed loss after drop: 13 km/h

Operation features:
- Airplane has a wide automatization of the engine systems, in fact, to control speed it is only necessary to use the throttle lever. There is no need to manually set engine revolutions and mixture or supercharger gear in normal flight. The engine supercharger has an automatic switch system which depends on altitude and engine revolutions.
- To reduce swinging during taxiing due to prop-wash the propeller pitch control should be switched to manual mode and pitch should be reduced to minimum.
- When the angle of attack increases to critical levels the wing may stall suddenly and unexpectedly. There is almost no pre-stall buffet before the stalling. To avoid this the pilot must pay additional attention when performing extreme maneuvering.
- Airplane has no flight-control trimmers. Airplane is equipped with bendable trim tabs that can be set pre-flight by ground personnel.
- Airplane has a manually controlled horizontal stabilizer which is electrically-actuated. It should be set to +1.5° 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.
- Airplane has electrically-actuated landing flaps with three fixed positions: retracted, takeoff (13°) and landing (58°). Flaps control buttons and indicator lights are located on left panel near the throttle. The flap angle may also be checked by indicators on the left and right wing outside the cockpit.
- Airplane has a tail wheel lock system which locks the tail wheel if the flight-stick is pulled backward. The tailwheel should be locked when taxiing straight for a long distance, before takeoff and after touchdown upon landing.
- Airplane has independent left and right hydraulic wheel brake controls. To apply either brake push the upper part of the rudder pedal.
- Airplane has a fuel gauge which shows the amount of remaining fuel in the front or rear fuel tank depending on switch position. In game the fuel indicator switch changes by itself during horizontal flight by every 10 seconds. Also, the airplane has an emergency fuel warning light (100 liters).
- It is impossible to open or close the canopy at high speed due to strong airflow. The canopy has an emergency release system for bailouts.
- The control system for the bomb rack only allows for dropping bombs one by one.
- The gunsight has a sliding sun-filter.
OLt. Zimmermann
Gruppenkommandeur

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