Ju 88 A-4

The Ju 88 A-4 is a German multirole bomber available as part of Battle of Moscow.

Specifications
 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 Configurations
 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