LaGG-3 ser.29 / IL-2 Sturmovik: Great Battles
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Fighter
LaGG-3 ser.29
History
Specifications

By the end of the 1930s, wood was considered an inferior material in aviation, and all-metal aircraft were gradually replacing those made of wood. Nevertheless, Lavochkin and Gorbunov, as well as Gudkov, who participated in the competition for a new Soviet fighter, had a realistic view of the possibilities of the aluminum industry in the USSR, so the I-301 fighter they designed, which was first flown on March 28, 1940, had a mixed construction with extensive use of wood.

The most important structural elements used delta wood, a wood composite made by pressing resin-impregnated veneer. Delta wood was stronger than ordinary wood, non-flammable, and resistant to rot. However, its production required the purchase of chemical plasticizer components from abroad, with most supplies coming from Germany. At the start of the war, this caused immediate problems.

The aircraft was tested quite successfully and was named LaGG-1. After the fuel supply was increased, mass production began in 1941. The wooden wing of the LaGG-3 with plywood skin was generally similar to the wing of the Yak-1 fighter. The difference was that in response to military demands, which Yakovlev ignored, the designers made the wing detachable. This solution greatly facilitated transportation, field repairs, and recovery of downed aircraft from forced landings at the cost of complicating the design and increasing the weight.

In 1942, the production of the 29th series began, the design of which was modified to take into account the combat experience of the first year of the war.

The LaGG-3 of the 29th series was a single-seat monoplane fighter of mixed construction with a low-slung wing, a water-cooled engine designed by Klimov, and an enclosed cockpit. The fuselage consisted of a metal forward truss and a wooden monocoque built as a single unit with a tail fin. The entire wooden structure was glued together. The 29th series was equipped with more powerful M-105PF engines with an output of 1210 hp and reduced altitude. For the M-105PF, the optimum altitude at which it developed maximum power was only 2700 meters — according to the experience of the battles on the Eastern Front, aircraft operated at low altitudes. At an altitude of 700 meters, the M-105PF developed 1260 hp.

Externally, the 29th series aircraft could be distinguished by three exhaust stacks, which replaced the single exhaust stack common to previous production aircraft. Along with the exhaust stack, the lining that protected the fighter's skin from hot exhaust gases disappeared from the aircraft's structure. Otherwise, the LaGG-3 of the 29th series did not differ in any way from the machines of the previous series.

The armament consisted of one cannon and one large-caliber machine gun.

Feedback on the LaGG-3 was quite contradictory: it had a strong and durable design, but it was too heavy for the engine installed on the machine. It should be noted that the LaGG-3 was designed as a heavy fighter to fight bombers but was used as a front-line fighter, and in this role was inferior in effectiveness to the Yakovlev light fighters. In the skillful hands of experienced pilots, the LaGG-3, especially the lightweight versions, fought successfully against fighters. The famous Soviet ace G.D. Kostylev flew the LaGG-3 successfully against the Germans and Finns from 1941 to 1943, shooting down almost 30 enemy planes. P.M. Kamozin also earned the title of Hero of the Soviet Union while flying the LaGG-3.

Sources used:

1. Yakubovich N. "Lavochkin's Airplanes" 2002.

2. Ivanov S. "LaGG-3" War in the air. №68

3. Kudrin N. "LaGG-3 - "dark horse"" Journal "Wings of the Motherland", No. 5, 1999.

4. Materials of the site airwar.ru

Indicated stall speed in flight configuration: 163..189 km/h
Indicated stall speed in takeoff/landing configuration: 138..168 km/h
Dive speed limit: 750 km/h
Maximum load factor: 11 G
Stall angle of attack in flight configuration: 18 °
Stall angle of attack in landing configuration: 15 °
 
Maximum true air speed at sea level, engine mode - Nominal: 505 km/h
Maximum true air speed at 2000 m, engine mode - Nominal: 548 km/h
Maximum true air speed at 4000 m, engine mode - Nominal: 573 km/h
 
Service ceiling: 10500 m
Climb rate at sea level: 14.9 m/s
Climb rate at 3000 m: 13.3 m/s
Climb rate at 6000 m: 8 m/s
 
Maximum performance turn at sea level: 22.2 s, at 280 km/h IAS.
Maximum performance turn at 3000 m: 28.9 s, at 270 km/h IAS.
 
Flight endurance at 3000 m: 2.2 h, at 350 km/h IAS.
 
Takeoff speed: 165..200 km/h
Glideslope speed: 200..210 km/h
Landing speed: 140..160 km/h
Landing angle: 12.8 °
 
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-105PF
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: 90..100 °C
Water maximum temperature in engine output: 110 °C
Oil rated temperature in engine output: 90..100 °C
Oil maximum temperature in engine output: 115 °C
 
Supercharger gear shift altitude: 2500 m
 
Empty weight: 2620 kg
Minimum weight (no ammo, 10% fuel): 2773 kg
Standard weight: 3157 kg
Maximum takeoff weight: 3701 kg
Fuel load: 348 kg / 467 l
Useful load: 1081 kg
 
Forward-firing armament:
20mm gun "SsVAK", 160 rounds, 800 rounds per minute, nose-mounted
12.7mm machine gun "UB", 200 rounds, 1000 rounds per minute, synchronized
23mm gun "VYa-23", 90 rounds, 600 rounds per minute, nose-mounted (modification)
37mm gun "Sh-37", 20 rounds, 185 rounds per minute, nose-mounted (modification)
 
Bombs:
2 x 50 kg general purpose bombs "FAB-50sv"
2 x 104 kg general purpose bombs "FAB-100M"
 
Rockets:
6 x 7 kg rockets "ROS-82", HE payload mass 2.52 kg
 
Length: 8.84 m
Wingspan: 9.8 m
Wing surface: 17.51 m²
 
Combat debut: May 1942
 
Operation features:
- The engine has a two-stage mechanical supercharger which must be manually switched at 2500m 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 aircraft has trimmers for all flight-controls: pitch, roll and yaw.
- Landing flaps have a hydraulic actuator and they can be extended to any angle up to 60°.
- The aircraft tailwheel rotates freely and does not have a lock. For this reason, it is necessary to confidently and accurately operate the rudder pedals during the takeoff and landing.
- 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.
- The aircraft has a fuel gauge which shows total remaining fuel.
- Cockpit canopy has a weak lock when in the opened position, for this reason the canopy may spontaneously close in a deep dive. It is impossible to open or close the canopy at high speed due to strong airflow. The canopy has no emergency release, so bail out requires the speed drop before it.
- The control system for the bomb rack only allows to drop the two bombs at the same time.
- When rockets are installed there is a salvo controller, it has three launch modes: single fire, fire two in a salvo or fire four in a salvo.
 
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 oil radiator control handle: open
- recommended position of the water radiator control handle: close
- recommended position of the prop pitch control handle: 100%
- recommended position of the throttle lever: 10%
 
2. Recommended mixture control lever positions for various flight modes:
- When running the engine at low throttle near the ground, the mixture knob should be in the position of about 50%.
- When the engine is running at full throttle near the ground, the mixture knob 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: 2.7 l/min
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