U-2VS / IL-2 Sturmovik: Great Battles
Close
menu
Transport
U-2VS
History
Specifications

Developed under the leadership of N.N. Polikarpov and renamed Po-2 after his death in 1944, the U-2, which made its first flight on January 7, 1928, was designed for the initial training of pilots. Its design was simple, but it had outstanding flight characteristics — easy to control, difficult to enter and easy to recover from a spin, predictable behavior at high angles of attack and low landing speed. The U-2 was easy to fly, and accidents could only happen for unwarranted reasons. More than a generation of future aces of the Red Army Air Force trained on it. The aircraft was so successful that it was used for training, communications, light transport, agriculture, passenger transport, etc., up to the famous night bomber of the Great Patriotic War. Movies were made about it, books were written about it, its fame crossed all borders. In 1941, a military modification of the U-2VS was introduced, designed to perform the tasks of a multipurpose light bomber, primarily a night bomber.

The U-2VS was a biplane with an air-cooled engine. The structure was made of pine and plywood with fabric covering, and the components were made of light metal. Beginning in 1942, in order to conserve materials, the wing tips, tail units, and landing gear fairings were made of wood and plywood, and the engine cowlings of sheet metal. In mid-1943, a new instrument panel was introduced with an attitude indicator, navigation lights were fitted, and a landing light was installed.

The star-shaped, air-cooled M-11D engine had a takeoff power of 125 hp and developed 105 hp at an altitude of 1000 m. Most of the aircraft were equipped with factory-made (or partially home-made) exhaust shrouds.

The armament included a defensive turret machine gun of rifle caliber, and sometimes a second one was fitted in a fixed position on top of the right wing panel — it was fed from an ammunition box installed in the fuselage. The aircraft could carry six 50 kg bombs or three 100 kg bombs.

With good horizontal maneuverability and low speed, the U-2VS was an extremely difficult target for enemy fighters at low altitude, which explains its relatively high combat survivability. When used as a night bomber, the U-2VS was difficult to detect above 5,000 feet (1,500 m), and with exhaust shrouds installed, at altitudes above 5,000-6,000 feet (700-800 m).

The low speed also made it possible to increase bombing accuracy. As one participant in the Battle of Stalingrad recalled: "Not a single modern night bomber can be given the kind of missions that the U-2 is given. They are given the task of bombing a house - a specific house, not to the left or the right, but exactly the one where the Germans are holed up. They are given the task of bombing the German half of the block, while the other half is in our hands. And with their low speed, with their ideal bombing target, they do the job... they bomb this particular house."

The famous "Night Witches" of the all-female 46th Guards Night Bomber Aviation Regiment flew the U-2VS.

Used sources:

V. Shavrov “History of aircraft designs in the USSR 1938-1950.” 1988

V. Shavrov “History of aircraft designs in the USSR until 1938” 1985

Materials from the site airwar.ru

Materials from the site life.ru

Indicated stall speed in flight configuration: 63..70 km/h
Dive speed limit: 240 km/h
Maximum load factor: 6.5 G
Stall angle of attack in flight configuration: 19°
 
Maximum true air speed at sea level, engine mode - Takeoff, 1750 RPM: 151.7 km/h
Maximum true air speed at 500 m, engine mode - Takeoff, 1740 RPM: 150.3 km/h
Maximum true air speed at 1000 m, engine mode - Takeoff, 1730 RPM: 148.9 km/h
 
Service ceiling: 3700 m
Climb rate:
500 m —  3 min. 5 sec.
1000 m — 6 min. 35 sec.
1500 m — 10 min. 40 sec.
2000 m — 15 min. 24 sec.
2500 m — 21 min. 15 sec.
3000 m — 28 min. 35 sec.
3500 m — 38 min. 20 sec.
 
Maximum performance turn: 22..23 s, at 105..115 km/h IAS.
 
Flight endurance at 500 m: 5 h, at 90 km/h IAS, 1300 RPM.
 
Takeoff speed: 75..85 km/h
Glideslope speed: 100 km/h
Landing speed: 60..70 km/h
Landing angle: 12°
 
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 full-throttle mode and 95 km/h IAS.
Note 5: turn rate is given for 1400..1500 RPM with roll 43°..45°.
 
Engine:
Model: M-11D
 
Maximum power in Takeoff mode (1750 RPM) at sea level: no less than 125 HP
 
Maximum power in Nominal mode (1700 RPM) at sea level: 118 HP
Maximum power in Nominal mode (1700 RPM) at 500 m: 110 HP
Maximum power in Nominal mode (1700 RPM) at 1000 m: 105 HP
 
Maximum power in Continuous mode (1640 RPM) at sea level: 107 HP
Maximum power in Continuous mode (1640 RPM) at 500 m: 100 HP
Maximum power in Continuous mode (1640 RPM) at 1000 m: 95 HP
 
Engine modes:
Takeoff/Emergency (5 min) : 1750/1840 RPM
Continuous/Nominal (unlimited): 1640/1700 RPM
 
Oil rated temperature in engine output: 70..80 °C
Oil maximum temperature in engine output: 115 °C
 
Airscrew:
Type 257, D 2.4 m, pitch 1.524 m
 
Empty weight: 748 kg
Minimum weight (no ammo, 10% fuel): 927 kg
Standard weight: 1007 kg
Maximum takeoff weight: 1350 kg
Fuel load: 90 kg / 126 l
Useful load: 350 kg
 
Forward-firing armament:
1 x 7.62mm machine gun "ShKAS", 500 rounds, 1800 rounds per minute, wing-mounted (modification)
 
Defensive armament:
Rear-facing: 7.62mm machine gun "ShKAS", 400 rounds, 1800 rounds per minute (modification)
 
Bombs:
2 x 50 kg general purpose bombs "FAB-50sv"
4 x 50 kg general purpose bombs "FAB-50sv"
6 x 50 kg general purpose bombs "FAB-50sv"
2 x 104 kg general purpose bombs "FAB-100M"
2 x 50 kg general purpose bombs "FAB-50sv" and 2 x 104 kg general purpose bombs "FAB-100M"
 
Height: 2.9 m
Length: 8.17 m
Wingspan of upper wing: 11.4 m
Wingspan of lower wing: 10.65 m
Wing surface: 33.15 m²
 
The U-2 aircraft was developed under N.N. Polikarpov supervision in 1923-1928. It was designed as a simple, sturdy, and easy to handle two-seater aircraft for flight schools. It went airborne for the first time on June 24, 1927, but many improvements to its design were made afterwards to improve its climb rate. The upgraded plane went into production in 1929 after the first flight on January 7, 1928.
 
Flight instructors and pilot candidates liked the plane - it forgave the typical mistakes of the trainees, was hard to stall and easy to recover, predictable at high angles of attack and had a low landing speed. Many future aces learned to fly in this \'flying school-desk\'. It was the first aircraft for the majority of VVS pilots.
 
Several modifications of this aircraft were developed: ambulance S-1 and S-2, passenger U-2SP and U-2L, agriculture U-2AP and military U-2VS. The military modification could carry up to 300 kg of bombs and was equipped with a defensive MG turret. During WWII, it was mainly used as a low-altitude bomber and recon plane. It was a very hard target for enemy fighters at low altitudes because of its low speed, resulting in its relatively high survivability rate. It was used by the famous "night witches", female pilots and navigators of 46th Guards night bomber regiment. The model was renamed to Po-2 to honor N.N. Polikarpov after his passing in 1944.
 
Operational features:
- There is no engine supercharger.
- The fuel mixture control is manual: the mixture should be leaned as the altitude increases for optimal engine functioning and to reduce the fuel consumption while flying level.
- The fixed pitch propeller requires controlling the engine RPM manually.
- The tail skid is linked to the rudder (8° maximum tilt).
- There are no wheel brakes.
- There is no electric generator in the default aircraft configuration, so electric lights and Pitot tube warmer (which consumes up to 226W) are fed from 24V battery (10 Ah capacity at 1 A current in standard conditions). To power the RSI-4 radio station, GS-10-350 electric generator is installed along with it.
- Please note that with all possible modifications and full fuel the total aircraft weight is 1390 kg, more than its maximum takeoff weight.
 
Basic data and recommended positions of the aircraft controls:
1. Starting the engine:
- recommended position of the mixture control lever: 100%
- recommended position of the radiator/cowl flap control handle: no radiator control
- recommended position of the prop pitch control handle: no prop pitch control
- recommended position of the throttle lever: 20%
 
2. Recommended mixture control lever positions for various flight modes:
- When running the engine at low throttle near the ground, the mixture control lever should be in the position of about 50%.
- When the engine is running at full throttle near the ground, the mixture control lever should be in the 75-80% position.
- As you gain altitude, the altitude corrector closes.
 
3. Recommended positions of the radiator/cowl flap control handle for various flight modes:  no control of radiators/cowl flaps
 
4. Approximate fuel consumption at 2000 m altitude:
- Cruise engine mode: 0.6 l/min
- Combat engine mode: 0.7 l/min
Up