IL-2 COMPARE ONLINE

GRAPH UNITSmetric

PLANE A & B per Fuel Load

Plane A Plane B

I.A.R.P.11f 1936 4.10.1m HSFX 5.00I-153 (2xBS) 1940 4.10.1m HSFX 5.00I-153 (Finland) 1940 4.10.1m HSFX 5.00I-15M-22 1934 4.10.1m HSFX 5.00I-15M-25 1937 4.10.1m HSFX 5.00I-16 Type 10 1937 4.10.1m HSFX 5.00I-16 Type 17 1938 4.10.1m HSFX 5.00I-16 Type 18 (2xBS) 1939 4.10.1m HSFX 5.00I-16 Type 27 1939 4.10.1m HSFX 5.00I-16 Type 28 1939 4.10.1m HSFX 5.00I-53 (BS 2xSHKAS) 1940 4.10.1m HSFX 5.00J7W1 1945 4.10.1m HSFX 5.00Jeep 1939 4.10.1m HSFX 5.00Ju-52-3mg6e 1939 4.10.1m HSFX 5.00Ju-88C-6 1942 4.10.1m HSFX 5.00Ki-43-III Ko 1944 4.10.1m HSFX 5.00Ki-44-II Ko 1942 4.10.1m HSFX 5.00

I.A.R.P.11f 1936 4.10.1m HSFX 5.00I-153 (2xBS) 1940 4.10.1m HSFX 5.00I-153 (Finland) 1940 4.10.1m HSFX 5.00I-15M-22 1934 4.10.1m HSFX 5.00I-15M-25 1937 4.10.1m HSFX 5.00I-16 Type 10 1937 4.10.1m HSFX 5.00I-16 Type 17 1938 4.10.1m HSFX 5.00I-16 Type 18 (2xBS) 1939 4.10.1m HSFX 5.00I-16 Type 27 1939 4.10.1m HSFX 5.00I-16 Type 28 1939 4.10.1m HSFX 5.00I-53 (BS 2xSHKAS) 1940 4.10.1m HSFX 5.00J7W1 1945 4.10.1m HSFX 5.00Jeep 1939 4.10.1m HSFX 5.00Ju-52-3mg6e 1939 4.10.1m HSFX 5.00Ju-88C-6 1942 4.10.1m HSFX 5.00Ki-43-III Ko 1944 4.10.1m HSFX 5.00Ki-44-II Ko 1942 4.10.1m HSFX 5.00

100% Fuel Load 100% Fuel Load

General Flight Model Data

Description Plane A Plane B unitsNo. Crew .............................. 1 1 countWing Area ............................. 21.4 21.4 sqr m.Weight Empty .......................... 2452.0 2452.0 kg.Weight Fuel Max ....................... 400.0 400.0 kg.Weight Engine ......................... 623.4 623.4 kg.Weight Takeoff ........................ -999 -999 kg.Weight Takeoff Max (ref only) ......... 2725.0 2725.0 kg.No. Engines ........................... 1 1 countNo. Super Charger Shift Levels ........ 2 2 countSuper Charger Shift Altitude 1 ........ 2850.0 2850.0 m.Super Charger Shift Altitude 2 ........ 6000.0 6000.0 m.Super Charger Shift Altitude 3 ........ n/a n/a m.Engine Scale Factor WEP ............... 1.1 1.1 countEngine Scale Factor BOOST ............. 1.05 1.05 countEngine Horse Power MIL ................ 1039.0 1039.0 Watts.Engine Horse Power WEP ................ 1142.9 1142.9 Watts.Engine Horse Power WEP+BOOST .......... 1200.045 1200.045 Watts.Thrust (Jets Only) .................... n/a n/a NewtonAoA Critical .......................... 20.0 20.0 deg.AoA Critical H at min flaps ........... 17.0 17.0 deg.AoA Critical H at max flaps ........... 15.0 15.0 deg.AoA Critical L at min flaps ........... -15.0 -15.0 deg.AoA Critical L at max flaps ........... -20.0 -20.0 deg.Best Turn Time at SL .................. 15.0 15.0 secBest Turn Speed at SL ................. 290 290 kphBest Climb Speed at SL ................ 220 220 kphVmin aka Stall Speed (TAS) ............ 150 150 kph

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Vmax at SL (TAS) ...................... 453 453 kphVmax (TAS) ............................ 560 560 kphVmax Allowed aka Vne (TAS) ............ 630 630 kphVmin Combat Flaps (TAS) ............... 125 125 kphVmin Landing Flaps (TAS) .............. 108 108 kphVmax Landing Flaps (TAS) .............. 250 250 kphFlaps Angle ........................... 12.0 12.0 deg.Flaps Multi ........................... 1.0 1.0 deg.

ROC & TAS per Power Selection

Plane A Plane B

WEP WEP

MIL MIL

Plane A Best Climb Angle Plane B Best Climb Angle

14.04 14.04

LEVEL TURN TIMES & RATE per Flap Setting at 1,000m (3,281ft)

Plane A Plane B

NONE NONE

COMBAT COMBAT

LANDING LANDING

TAKE OFF TAKE OFF

FLIGHT MODEL PARAMETERS per Percent Flap Settings

Plane A Plane B

NONE NONE

20% 20%

40% 40%

60% 60%

80% 80%

100% 100%

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