il2

Li-2

li2

Description

Indicated stall speed in flight configuration: 115…135 km/h
Indicated stall speed in takeoff/landing configuration: 105…120 km/h
Dive speed limit: 410 km/h
Maximum load factor: 5.0 G
Stall angle of attack in flight configuration: 13 °
Stall angle of attack in landing configuration: 12.5 °

Maximum true air speed at sea level, engine mode - take-off: 322 km/h
Maximum true air speed at 900 m, engine mode - take-off: 333 km/h

Maximum true air speed at sea level, engine mode - economical maximum: 303 km/h
Maximum true air speed at 1700 m, engine mode - economical maximum: 320 km/h

Service ceiling: 5500 m
Climb rate at sea level: 4,0 m/s
Climb rate at 3000 m: 2,5 m/s

Maximum performance turn at sea level: 25.5 s, at 220 km/h IAS.

Flight endurance at 4000 m: 9h, at 2000 rpm / 640 mm Hg MAP

Takeoff speed: 120..130 km/h
Glideslope speed: 150..165 km/h
Landing speed: 105..115 km/h
Landing angle: 11.5 °

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 maximum continuous power, turn times are given for nominal power.

Engine:
Model: M-62IR
Maximum power in take-off mode at sea level: 1000 HP
Maximum power in maximum continuous (nominal) mode at sea level: 820 HP

Maximum power in maximum continuous (nominal) mode at 1700 m: 840 HP

Engine modes:
Take-off (up to 5 minutes): 2200 RPM, 1050 mm Hg
Nominal: 2100 RPM, 900 mm Hg

Oil rated temperature in engine output: 115 °C
Oil maximum temperature in engine output: 125 °C
Cylinder head rated temperature: 205 °C
Cylinder head maximum temperature: 235 °C

Empty weight: 7526 kg
Maximum takeoff weight: 11600 kg
Fuel load: 2240 kg / 3110 l
Useful load: 4074 kg

Forward-firing armament:
7.62 mm “ShKAS” machine gun, 450 rounds, 1800 rounds per minute, nose-mounted

Defensive armament:
Top: 12.7 mm machine gun “UBT” in UTK-1 turret, 230 rounds, 1000 rounds per minute
Left: 7.62 mm “ShKAS” machine gun, 500 rounds, 1800 rounds per minute
Right: 7.62 mm “ShKAS” machine gun, 500 rounds, 1800 rounds per minute

Bombs:
Up to 4 x 254 kg general purpose bombs “FAB-250sv”
Up to 2 x 512 kg general purpose bombs “FAB-500M”

Length: 19.65 m
Wingspan: 28,81 m
Wing surface: 91,7 m²

Combat debut: Autumn 1942

Operation features:

Basic data and recommended positions of the aircraft controls:

  1. Starting the engine:
    • recommended position of the mixture control lever: forward
    • recommended position of the cowl flap control handle: close
    • recommended position of the radiator control handle: open 50%
    • recommended position of the prop pitch control handle: heavy
    • recommended position of the throttle lever: 15%
    • before taxiing, you must unlock the tailwheel
    • before taxiing, the parking brake must be released
  2. Recommended mixture control lever positions for various flight modes:
    • When running the engine at low throttle near the ground, the mixture control lever should be in the position of about 60%.
    • When the engine is running at full throttle near the ground, the mixture control lever should be in the 40-50% position.
    • As you gain altitude, the altitude corrector closes.

3.1 Recommended positions of the radiator/cowl flap control handle for various flight modes: / no control of radiators/cowl flaps
- takeoff: open 100%
- climb: open 100%
- cruise flight: open 50% (in winter conditions - close if necessary)
- combat: open 50%

3.2 Recommended positions of the radiator/cowl flap control handle for various flight modes: / no control of radiators/cowl flaps
- takeoff: open 50%
- climb: open 100%
- cruise flight: open 40% (in winter conditions - close if necessary)
- combat: open 50%

  1. Approximate fuel consumption at 2000 m altitude:
    • Cruise engine mode: 7.7 l/min
    • Combat engine mode: 9.8 l/min

Modifications

16 paratroopers
16 paratroopers with equipment
Additional mass: 1600 kg
Estimated speed loss before drop: 7 km/h
Estimated speed loss after drop: 0 km/h

Bomb Load
4 x 254 kg General Purpose Bombs FAB-250sv
Additional mass: 1076 kg
Ammunition mass: 1016 kg
Racks mass: 60 kg
Estimated speed loss before drop: 13 km/h
Estimated speed loss after drop: 2 km/h
or
2 x 512 kg General Purpose Bombs FAB-500M
Additional mass: 1084 kg
Ammunition mass: 1024 kg
Racks mass: 60 kg
Estimated speed loss before drop: 17 km/h
Estimated speed loss after drop: 2 km/h

6 x PD-MM containers
6 x 125 kg drop transport container with parachute PD-MM
Additional mass: 814 kg
Containers mass: 754 kg
Racks mass: 60 kg
Estimated speed loss before drop: 20 km/h
Estimated speed loss after drop: 2 km/h

14 PD-MM containers (inside)
14 x 125 kg drop transport container with parachute PD-MM stored in the cargo compartment
Additional mass: 1760 kg
Estimated speed loss before drop: 5 km/h
Estimated speed loss after drop: 0 km/h

2200 kg of cargo
2200 kg of military cargo payload
Additional mass: 2200 kg
Estimated speed loss: 6 km/h