Indicated stall speed in flight configuration: 165..183 km/h
Indicated stall speed in takeoff/landing configuration: 147..162 km/h
Dive speed limit: 720 km/h
Maximum load factor: 10 G
Stall angle of attack in flight configuration: 22.7 °
Stall angle of attack in landing configuration: 15.1 °
Maximum true air speed at sea level, engine mode - Boosted: 550 km/h
Maximum true air speed at 3000 m, engine mode - Boosted: 575 km/h
Maximum true air speed at 6200 m, engine mode - Nominal: 595 km/h
Service ceiling: 9700 m
Climb rate at sea level: 19 m/s
Climb rate at 3000 m: 14.0 m/s
Climb rate at 6000 m: 8.8 m/s
Maximum performance turn at sea level: 21.7 s, at 290 km/h IAS.
Maximum performance turn at 3000 m: 32.0 s, at 300 km/h IAS.
Flight endurance at 3000 m: 1.9 h, at 350 km/h IAS.
Takeoff speed: 170..200 km/h
Glideslope speed: 200..210 km/h
Landing speed: 150..160 km/h
Landing angle: 13 °
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 Boosted power.
Engine:
Model: M-82
Maximum power in Boosted mode at sea level: 1700 HP
Maximum power in Nominal mode at sea level: 1400 HP
Maximum power in Nominal mode at 2100 m: 1550 HP
Maximum power in Nominal mode at 5300 m: 1335 HP
Engine modes:
Nominal (unlimited time): 2400 RPM, 950 mm Hg
Boosted power (up to 5 minutes): 2400 RPM, 1140 mm Hg
Oil rated temperature in engine output: 55..90 °C
Oil maximum temperature in engine output: 125 °C
Cylinder head rated temperature: 140..210 °C
Cylinder head maximum temperature: 250 °C
Supercharger gear shift altitude: 3500 m
Empty weight: 2648 kg
Minimum weight (no ammo, 10% fuel): 2928 kg
Standard weight: 3353 kg
Maximum takeoff weight: 3593 kg
Fuel load: 370 kg / 521 l
Useful load: 945 kg
Forward-firing armament:
2 x 20mm gun “SsVAK”, 170 rounds, 800 rounds per minute, synchronized
Bombs:
2 x 50 kg general purpose bombs “FAB-50sv”
2 x 104 kg general purpose bombs “FAB-100M”
Length: 8.672 m
Wingspan: 9.8 m
Wing surface: 17.51 m²
Combat debut: September 1942
Operation features:
Basic data and recommended positions of the aircraft controls:
3.1 Recommended positions of cowl flaps for various flight modes:
- takeoff: open
- climb: open
- cruise flight: open (in winter conditions - close 50% if necessary)
- combat: open
3.2 Recommended positions of cowl flaps for various flight modes:
- takeoff: open 100%
- climb: open 100%
- cruise flight: open 20% (in winter conditions - close if necessary)
- combat: open 60%
3.3 Recommended positions of the oil radiator control handle for various flight modes:
- takeoff: open 50%
- climb: open 100%
- cruise flight: open 20% (in winter conditions - close if necessary)
- combat: open 50%
2 x FAB-50sv bombs
2 x 50 kg General Purpose Bombs FAB-50sv
Additional mass: 120 kg
Ammunition mass: 100 kg
Racks mass: 20 kg
Estimated speed loss before drop: 20 km/h
Estimated speed loss after drop: 12 km/h
RPK-10
Fixed loop radio compass for navigation with radio beacons
Additional mass: 10 kg
Estimated speed loss: 0 km/h
Special Guns Ammo Load
Loadout variants: armour piercing (AP) or high-explosive (HE) rounds only
2 x FAB-100M bombs
2 x 104 kg General Purpose Bombs FAB-100M
Additional mass: 228 kg
Ammunition mass: 208 kg
Racks mass: 20 kg
Estimated speed loss before drop: 27 km/h
Estimated speed loss after drop: 12 km/h
M-82F engine
Late M-82F engine modification with unlimited boosted mode duration.
Additional mass: 0 kg
Estimated speed loss: 0 km/h
Flat Windscreen
Flat frontal section for better visibility
Additional mass: 2 kg
Estimated speed loss: 2 km/h