La-5FN Series 2 / IL-2 Sturmovik: Great Battles
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Fighter
La-5FN Series 2
History
Specifications

The La-5 fighter was introduced in 1942 when a more powerful air-cooled M-82 engine was installed on the LaGG-3 fighter's airframe instead of a water-cooled engine. Even with the new engine, the aircraft was inferior in performance to the main German fighters, so the Shvetsov Design Bureau worked on increasing the engine's power, and in 1943 an improved version with direct fuel injection went into production. The plane with this engine was first flown on March 15, 1943, and immediately went into production. From series to series, the La-5FN was constantly improved.

The second series La-5FN was a single-engine wooden low-wing aircraft. Like the LaGG-3 and previous La-5 modifications, the main structural material of the airframe was pine. Delta wood was used for wing spars and some frames. The wooden parts of the aircraft were glued together. The fuselage consisted of a metal front frame and a wooden monocoque, which was made in one piece with the tail. The pilot's cockpit was closed by a sliding canopy that locked in the open and closed positions - the Series 2 aircraft did not have an emergency canopy release mechanism. Externally, the aircraft differed from the La-5F by a new compressor air intake and new openings for the engine cooling system. The canopy flaps were mounted on a piano hinge in the upper part, next to the supercharger air intake, and there was a heat-resistant panel on the side of the fuselage. In this series, the elevator area was increased, changes were made to the lateral control system, and several other minor changes were made.

The M-82FN engine developed a maximum ground-level power of 1850 hp in boosted mode and 1460 hp at an altitude of 4800 m in nominal mode. The armament remained unchanged and consisted of 2 synchronized 20 mm ShVAK cannons; if necessary, 2 bomb racks for carrying bombs of 50 or 100 kg could be installed under the wing.

Military tests of the first series of new Lavochkin took place in the air battles over the Kursk Bulge. The good speed and excellent maneuverability of the fighter at low altitudes, where most of the battles on the Eastern Front took place, became an unpleasant surprise for the Luftwaffe. According to General A.S. Blagoveshchensky, commander of the 2nd Fighter Air Corps and later head of the Air Force Research Institute, the La-5FN was the best fighter in the Air Force in 1943. However, a carelessly made cockpit canopy, due to which the pilot might not have enough strength to move it in flight in the absence of an emergency release mechanism, as well as some manufacturing defects reduced the combat qualities of the plane.

However, the advantages of the aircraft outweighed its disadvantages and in 1944 3,826 La-5FN fighters were produced. If we take the ratio of enemy planes shot down to the number of losses as a criterion for the effectiveness of a fighter, we can consider the results of the 4th Air Army for 1944 as a reliable example. The La-5 flew 4,161 missions and took part in 270 air battles in which 177 enemy planes were shot down and 27 of their own were lost. The ratio of victories to losses is 6.55:1. For comparison, the same ratio for Yakovlev fighters was 4:1.

The La-5FN was quickly written off after the end of the war — the wooden structure of the aircraft was not suitable for long-term operation in peacetime conditions.

Czechoslovakia was the only country besides the USSR to operate La-5FN fighters. In the Czechoslovak Air Force, the La-5FN received the designation S-95 and continued to be used even after fighters of this type were retired in the USSR.

1. S. Ivanov “La-5” War in the air No. 69 2001

2. “La-5” magazine “Aircraft History” No. 1 2006

3. Materials from the site airwar.ru

Indicated stall speed in flight configuration: 168..185 km/h
Indicated stall speed in takeoff/landing configuration: 147..159 km/h
Dive speed limit: 720 km/h
Maximum load factor: 10 G
Stall angle of attack in flight configuration: 22.2 °
Stall angle of attack in landing configuration: 15.0 °
 
Maximum true air speed at sea level, engine mode - Nominal: 552 km/h
Maximum true air speed at sea level, engine mode - Boosted: 583 km/h
Maximum true air speed at 2500 m, engine mode - Nominal: 605 km/h
Maximum true air speed at 6000 m, engine mode - Nominal: 646 km/h
 
Service ceiling: 10500 m
Climb rate at sea level: 20 m/s
Climb rate at 3000 m: 16.7 m/s
Climb rate at 6000 m: 12.5 m/s
 
Maximum performance turn at sea level: 21.0 s, at 320 km/h IAS.
Maximum performance turn at 3000 m: 28.0 s, at 340 km/h IAS.
 
Flight endurance at 3000 m: 2.0 h, at 350 km/h IAS.
 
Takeoff speed: 175..195 km/h
Glideslope speed: 200..210 km/h
Landing speed: 150..160 km/h
Landing angle: 13 °
 
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 Boosted power.
 
Engine:
Model: M-82FN
Maximum power in Boosted mode at sea level: 1850 HP
Maximum power in Nominal mode at sea level: 1560 HP
Maximum power in Nominal mode at 1550 m: 1630 HP
Maximum power in Nominal mode at 4800 m: 1460 HP
 
Engine modes:
Nominal (unlimited time): 2400 RPM, 1000 mm Hg
Boosted power (up to 10 minutes): 2500 RPM, 1180 mm Hg
 
Oil rated temperature in engine intake: 65..75 °C
Oil maximum temperature in engine intake: 85 °C
Cylinder head rated temperature: 180..215 °C
Cylinder head maximum temperature: 250 °C
 
Supercharger gear shift altitude: 3500 m
 
Empty weight: 2655 kg
Minimum weight (no ammo, 10% fuel): 2929 kg
Standard weight: 3305 kg
Maximum takeoff weight: 3544 kg
Fuel load: 334 kg / 464 l
Useful load: 896 kg
 
Forward-firing armament:
2 x 20mm gun "SsVAK", 170 rounds, 800 rounds per minute, synchronized
 
Bombs:
2 x 50 kg general purpose bombs "FAB-50sv"
2 x 104 kg general purpose bombs "FAB-100M"
 
Length: 8.672 m
Wingspan: 9.8 m
Wing surface: 17.51 m²
 
Combat debut: June 1943
 
Operation features:
- The engine has a boost mode. To engage it, increase the manifold pressure to 1180 mm Hg. Boost only works on 1st supercharger gear.
- The engine has a two-stage mechanical supercharger which must be manually switched at 3500m altitude.
- 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.
- Oil radiator, air cooling intake and outlet shutters are manually controlled.
- Air cooling intake shutters should always be open. They should only be closed when there is a possibility of engine overcooling, for example in a dive with idle throttle.
- The aircraft is equipped with elevator and rudder trimmers.
- The aircraft has automatic wing slats. They deploy when the high angle of attack increases which makes pre-stall softer.
- 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.
- Also, it is impossible to open or close 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.
 
Basic data and recommended positions of the aircraft controls:
1. Starting the engine:
- recommended position of the mixture control lever: no mixture control
- recommended position of the cowl flap control handle: open
- recommended position of the radiator/cowl flap control handle: close
- recommended position of the prop pitch control handle: 100%
- recommended position of the throttle lever: 0%
 
2. Recommended mixture control lever positions for various flight modes: no mixture control
 
3.1 Recommended positions of cowl flaps for various flight modes:
- takeoff: open
- climb: open
- cruise flight: open (in winter conditions - close 50% if necessary)
- combat: open
 
3.2 Recommended positions of cowl flaps for various flight modes:
- takeoff: open 100%
- climb: open 100%
- cruise flight: open 20% (in winter conditions - close if necessary)
- combat: open 60%
 
3.3 Recommended positions of the oil radiator control handle for various flight modes:
- takeoff: open 50%
- climb: open 100%
- cruise flight: open 20% (in winter conditions - close if necessary)
- combat: open 50%
4. Approximate fuel consumption at 2000 m altitude:
- Cruise engine mode: 3.6 l/min
- Combat engine mode: 12.3 l/min
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