P-40E-1

The P-40E-1 is an American fighter available as part of Battle of Moscow (Collector's Edition). It was delivered to the VVS as part of the Lend-Lease program.

Specifications
 Indicated stall speed in flight configuration: 153..176 km/h Indicated stall speed in takeoff/landing configuration: 141..164 km/h

Dive speed limit: 860 km/h Maximum load factor: 12.2 G Stall angle of attack in flight configuration: 14 ° Stall angle of attack in landing configuration: 12.6 °

Maximum true air speed at sea level, engine mode - Take-off: 494 km/h Maximum true air speed at 5000 m, engine mode - Take-off: 601 km/h

Service ceiling: 9200 m Climb rate at sea level: 12.5 m/s Climb rate at 3000 m: 10 m/s Climb rate at 6000 m: 3.7 m/s

Maximum performance turn at sea level: 24.3 s, at 270 km/h IAS. Maximum performance turn at 3000 m: 36.1 s, at 270 km/h IAS.

Flight endurance at 3000 m: 2.8 h, at 350 km/h IAS.

Takeoff speed: 160..190 km/h Glideslope speed: 210..220 km/h Landing speed: 140..145 km/h Landing angle: 13.9 °

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 Take-off power, turn times are given for Maximum possible power.

Engine: Model: V-1710-39 Maximum power in Maximum Possible power mode at sea level: 1470 HP Maximum power in Take-off mode at sea level: 1150 HP Maximum power in Nominal mode at sea level: 900 HP Maximum power in Combat mode at 12000 feet: 1150 HP Maximum power in Nominal mode at 10800 feet: 1000 HP

Engine modes: Nominal (unlimited time): 2600 RPM, 37.2 inch Hg Combat power (up to 5 minutes): 3000 RPM, 42 inch Hg Take-off power (up to 2 minutes): 3000 RPM, 45.5 inch Hg Maximum Possible power (prohibited by flight manual): 3000 RPM, 56.0 inch Hg

Water rated temperature in engine output: 105..115 °C Water maximum temperature in engine output: 125 °C Oil rated temperature in engine intake: 70..85 °C Oil maximum temperature in engine intake: 90 °C

Supercharger gear shift altitude: single gear

Empty weight: 3073 kg Minimum weight (no ammo, 10% fuel): 3264.2 kg Standart weight: 3819.1 kg Maximum takeoff weight: 4414 kg Fuel load: 404 kg / 561 l Useful load: 1341 kg

Forward-firing armament: 6 x 12.7mm machine gun "M2.50", 235 rounds, 850 rounds per minute, wing-mounted

Bombs: 254 kg general purpose bomb "FAB-250sv" 512 kg general purpose bomb "FAB-500M"

Rockets: 4 x 7 kg rockets "ROS-82", HE payload mass 2.52 kg

Length: 9.05 m Wingspan: 11.4 m Wing surface: 21.92 m^2

Combat debut: December 1941

Additional Configurations
 Removal of 2 external wing-mounted machine guns to reduce total weight Weight savings: 156 kg Removed ammunition mass: 64 kg Removed guns mass: 92 kg Estimated additional speed: 3 km/h

Additional ammo for machine guns: 312 for internal ones, 291 for middle ones, 240 for external ones (instead of 235 per each) or 615 per each for 4x MG. 6 machineguns: Additional mass: 38 kg Estimated speed loss: 0 km/h 4 machineguns: Additional mass: 207 kg Estimated speed loss: 2 km/h

254 kg General Purpose Bomb FAB-250sv Additional mass: 264 kg Ammunition mass: 254 kg Rack mass: 10 kg Estimated speed loss before drop: 19 km/h Estimated speed loss after drop: 7 km/h

254 kg General Purpose Bomb FAB-500M Additional mass: 522 kg Ammunition mass: 512 kg Rack mass: 10 kg Estimated speed loss before drop: 36 km/h Estimated speed loss after drop: 7 km/h

4 x 82mm High Explosive unguided rockets ROS-82 Additional mass: 40 kg Ammunition mass: 28 kg Racks mass: 12 kg Estimated speed loss before launch: 13 km/h Estimated speed loss after launch: 10 km/h