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

```