Yak-1b ser.127 / IL-2 Sturmovik: Great Battles
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Fighter
Yak-1b ser.127
History
Specifications

The design bureau of the Deputy People's Commissar for the Aircraft Industry Yakovlev was among those involved in creating a new generation of combat aircraft in the USSR, working on the I-26 project. The specialization of the design bureau, which had previously created sport aircraft, had a positive impact on the project. The fighter was to have high speed and maneuverability thanks to efficient aerodynamic design and a rational layout with all large masses near the center of gravity.

The prototype flew for the first time on January 13, 1940 and turned out to be "crude": the tests were accompanied by continuous failures, accidents, and even disasters. If Yakovlev had not been a deputy people's commissar, the story of this fighter would probably have ended at the factory testing stage, but due to the use of administrative resources, the aircraft, which was given the name Yak-1, not only entered state tests, but in 1940 was put into mass production even before they were carried out. As a result, it had several major defects, which, however, did not change its overall high rating. During production, the design was continually modified to reflect combat experience.

Serial production of the improved modification of the Yak-1B began in 1942 and ended only in June 1944: in September 1942, 10 aircraft were produced, and from October only the Yak-1B was produced.

The Yak-1B was a single-seat front-line fighter monoplane with a low wing of wooden construction and a retractable two-strut landing gear with a tail wheel that was also retractable. Some equipment was removed from the aircraft to lighten the structure, and internal sealing of the fuselage compartments was introduced. The fuselage was mounted on a welded metal frame that was integral with the engine mount.

Unlike earlier modifications, the cockpit canopy was teardrop-shaped, behind which the fuselage was cut down: this greatly improved visibility, especially to the rear. To prevent the canopy from being splashed with oil from the engine, which was a common problem, an oil deflector was installed. The protection of the pilot was improved by the installation of armored glass in front and behind his head.

The water-cooled M-105PF engine remained the same, but the propeller was replaced by a three-blade VISH-105 SV. The engine developed 1240 shp at takeoff and 1200 shp at an altitude of 4000 m.

The armament still included a 20 mm cannon mounted in the camber of the engine cylinder block, firing through the hollow shaft and propeller transmission, and the rifle-caliber machine guns were replaced by a large-caliber UBS machine gun above the left engine. Racks for two bombs of 50 or 100 kg could be fitted under the wings.

A total of 4,188 Yak-1b were built. Yak-1b series 127 appeared at the front in the spring of 1943.

Many famous Soviet aces flew the Yak-1b: Arseny Vorozheikin, Alexander Koldunov, Alexey Alelyukhin, Sergey Lugansky, and others; these fighters were also in service with the Normandy Squadron.

Transferred to the 296th Fighter Aviation Regiment (later 73rd Guards IAP), the famous pilot Lydia Litvyak flew the Yak-1B before being killed in action. Her call sign was "Lily" and a white lily was painted on her plane, so she went down in history as the “White Lily of Stalingrad.”

Although the Yak-1b was becoming obsolete and could not compete with the new modifications of the Messerschmitts and Focke-Wulfs, pilots and technicians still loved it. Despite the changes in design, it retained its simplicity and ease of operation and remained straightforward in maintenance.

Used sources:

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

M. Nikolsky “Yak-fighter” Aviation and Cosmonautics magazine No. 5-5 1999

Materials from the site airwar.ru

Indicated stall speed in flight configuration: 153..169 km/h
Indicated stall speed in takeoff/landing configuration: 132..145 km/h
Dive speed limit: 720 km/h
Maximum load factor: 10.3 G
Stall angle of attack in flight configuration: 18 °
Stall angle of attack in landing configuration: 15.6 °
 
Maximum true air speed at sea level, engine mode - Nominal, 2550 RPM: 530 km/h
Maximum true air speed at 2000 m, engine mode - Nominal, 2700 RPM: 567 km/h
Maximum true air speed at 4500 m, engine mode - Nominal, 2700 RPM: 600 km/h
 
Service ceiling: 10600 m
Climb rate at sea level: 17.0 m/s
Climb rate at 3000 m: 15.0 m/s
Climb rate at 6000 m: 9.5 m/s
 
Maximum performance turn at sea level: 19.0 s, at 270 km/h IAS.
Maximum performance turn at 3000 m: 24.1 s, at 270 km/h IAS.
 
Flight endurance at 3000 m: 2.0 h, at 350 km/h IAS.
 
Takeoff speed: 160..190 km/h
Glideslope speed: 195..205 km/h
Landing speed: 135..145 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 and turn times are given for Nominal (2700 RPM) power.
 
Engine:
Model: M-105PF
Maximum power in Nominal mode (2550 RPM) at sea level: 1240 HP
Maximum power in Nominal mode (2700 RPM) at sea level: 1210 HP
Maximum power in Nominal mode (2700 RPM) at 800 m: 1260 HP
Maximum power in Nominal mode (2700 RPM) at 2700 m: 1200 HP
 
Engine modes:
Nominal (unlimited time): 2550/2700 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: 2322 kg
Minimum weight (no ammo, 10% fuel): 2543 kg
Standard weight: 2887 kg
Maximum takeoff weight: 3117 kg
Fuel load: 304 kg / 408 l
Useful load: 795 kg
 
Forward-firing armament:
20mm gun "SsVAK", 140 rounds, 800 rounds per minute, nose-mounted
12.7mm machine gun "UB", 220 rounds, 1000 rounds per minute, synchronized
 
Bombs:
2 x 50 kg general purpose bombs "FAB-50sv"
2 x 104 kg general purpose bombs "FAB-100M"
 
Length: 8.5 m
Wingspan: 10 m
Wing surface: 17.15 m²
 
Combat debut: April 1943
 
Operation features:
- The engine has a two-stage mechanical supercharger which must be manually switched at 2300m altitude.
- Engine mixture control is manual; it is necessary to lean the mixture if altitude is more than 3-4 km for optimal engine operation. Also, leaning the mixture allows a reduction in fuel consumption during flight.
- Engine RPM has an automatic governor and it is maintained at the required RPM corresponding to the governor control lever position. The governor automatically controls the propeller pitch to maintain the required RPM.
- Water and oil radiator shutters are controlled manually.
- The airplane can only be trimmed in the pitch axis.
- Landing flaps have a pneumatic actuator. Flaps can only be fully extended; gradual extending is impossible. Due to the weak force of the actuator the extended landing flaps may be pressed upwards by the airflow if the airspeed is more than 220 km/h. Remember that the flaps will not extend fully in case of high speed. In case of a high-speed landing approach the flaps may extend a few steps further right before landing.
- The aircraft has a tailwheel control system which is unlocked by the rudder if the rudder pedal is pressed more than 75% of its range. The tailwheel remains locked if pedals are deflected less than 75%. Because of this, it is necessary to avoid large rudder pedal inputs when moving at high speed.
- The aircraft has differential pneumatic wheel brakes with shared control lever. This means that if the brake lever is held and the rudder pedal the opposite wheel brake is gradually released causing the plane to swing to one side or the other.
- Fuel gauges are installed on left and right wing fuel tanks, outside of the cockpit. They show remaining fuel level only when there is less than 80 liters of fuel left in the tank.
- The canopy has no emergency release. In order to bail out, you must slow below 550 kph to open the canopy.
- The control system for the wing-mounted bomb racks only allows releasing of both bombs together.
 
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 radiators control handles: close
- recommended position of the prop pitch control handle: 100%
- recommended position of the throttle lever: 5%
- before taxiing, you must unlock the tailwheel
 
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. At 8-9 km altitude, the altitude corrector closes to 0%.
 
3.1 Recommended positions of the oil radiator control handle for various flight modes:
- takeoff: open 100%
- climb: open 100%
- cruise flight: open 40%
- combat: open 100%
 
3.2 Recommended positions of the water radiator control handle for various flight modes:
- takeoff: open 100%
- climb: open 100%
- cruise flight: open 50%
- combat: open 80%
 
4. Approximate fuel consumption at 2000 m altitude:
- Cruise engine mode: 7.5 l/min
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