Pe-2 Series 87

The **Pe-2 Series 87** is a Russian bomber and attack aircraft available as part of *Battle of Stalingrad*.

## Specifications

```
Indicated stall speed in flight configuration: 175..200 km/h
Indicated stall speed in takeoff/landing configuration: 148..169 km/h
Dive speed limit: 790 km/h
Maximum load factor: 11 G
Stall angle of attack in flight configuration: 13.9 °
Stall angle of attack in landing configuration: 9.8 °

Maximum true air speed at sea level, engine mode - Nominal: 446 km/h
Maximum true air speed at 2000 m, engine mode - Nominal: 476 km/h
Maximum true air speed at 5000 m, engine mode - Nominal: 498 km/h

Service ceiling: 8000 m
Climb rate at sea level: 10.4 m/s
Climb rate at 3000 m: 7.8 m/s
Climb rate at 6000 m: 3.0 m/s

Maximum performance turn at sea level: 29.9 s, at 270 km/h IAS.
Maximum performance turn at 3000 m: 40.3 s, at 270 km/h IAS.

Flight endurance at 3000 m: 2.8 h, at 300 km/h IAS.

Takeoff speed: 160..200 km/h
Glideslope speed: 220..240 km/h
Landing speed: 155..165 km/h
Landing angle: 12.5 °

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 and turn times are given for Nominal power.

Engine:
Model: M-105RF
Maximum power in Nominal mode at sea level: 1200 HP
Maximum power in Nominal mode at 800 m: 1260 HP
Maximum power in Nominal mode at 2700 m: 1200 HP

Engine modes:
Nominal (unlimited time): 2700 RPM, 1050 mm Hg

Water rated temperature in engine output: 70..85 °C
Water maximum temperature in engine output: 100 °C
Oil rated temperature in engine output: 90..100 °C
Oil maximum temperature in engine output: 115 °C

Supercharger gear shift altitude: 2300 m

Empty weight: 6089 kg
Minimum weight (no ammo, 10% fuel): 6643 kg
Standard weight: 7685 kg
Maximum takeoff weight: 8701 kg
Fuel load: 1113 kg / 1484 l
Useful load: 2612 kg

Forward-firing armament:
12.7mm machine gun "UB", 150 rounds, 1000 rounds per minute, nose-mounted
7.62mm machine gun "ShKAS", 450 rounds, 1800 rounds per minute, nose-mounted

Defensive armament:
Top: 12.7mm machine gun "UB", 200 rounds, 1000 rounds per minute
Belly: 12.7mm machine gun "UB", 200 rounds, 1000 rounds per minute
Side: 7.62mm machine gun "ShKAS", 225 rounds, 1800 rounds per minute
Top turret: 12.7mm machine gun "UB", 200 rounds, 1000 rounds per minute (modification "series 110")

Bombs:
Up to 10 x 104 kg general purpose bombs "FAB-100M"
Up to 4 x 254 kg general purpose bombs "FAB-250sv"
Up to 2 x 512 kg general purpose bombs "FAB-500M"

Rockets:
10 x 23 kg rockets "ROS-132", HE payload mass 9.1 kg

Length: 12.69 m
Wingspan: 17.12 m
Wing surface: 40.8 m^2

Combat debut: May 1942

```

### Additional Configurations

```
10 x 104 kg General Purpose Bombs FAB-100M
Additional mass: 1040 kg
Ammunition mass: 1040 kg
Estimated speed loss before drop: 23 km/h
Estimated speed loss after drop: 0 km/h

4 x 254 kg General Purpose Bombs FAB-250sv
Additional mass: 1016 kg
Ammunition mass: 1016 kg
Estimated speed loss before drop: 33 km/h
Estimated speed loss after drop: 0 km/h

2 x 512 kg General Purpose Bombs FAB-500M
Additional mass: 1024 kg
Ammunition mass: 1024 kg
Estimated speed loss before drop: 48 km/h
Estimated speed loss after drop: 0 km/h

10 x 132mm High Explosive unguided rockets ROS-132
Additional mass: 280 kg
Ammunition mass: 230 kg
Racks mass: 50 kg
Estimated speed loss before launch: 31 km/h
Estimated speed loss after launch: 20 km/h

VUB-1 rear wide-angle turret with UBT 12.7mm machinegun with 200 rounds
Additional mass: 0 kg
Estimated speed loss: 5 km/h

```