La-5F ser.38 / IL-2 Sturmovik: Great Battles
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Fighter
La-5F ser.38
History
Specifications

The La-5 fighter was introduced in 1942 when a more powerful Shvetsov Design Bureau M-82 air-cooled engine was installed instead of a water-cooled engine on the airframe of the LaGG-3 fighter. The reasons for this are simple: the LaGG turned out to be heavier than the Yak, and the engines on the fighters were the same. At the same time, after the Su-2 was phased out, a large number of M-82 engines were produced for it, and their installation promised an increase of 300 hp. and increased survivability when bullets and cannon shells hit the engine. Although the drag of the aircraft increased due to the larger center section of the engine, the increase in power offset the increase in drag, allowing for greater speed and climb rate.

However, the La-5 was inferior to the Bf 109 F-4 and Bf 109 G-2 in both horizontal speed and climb rate, according to military tests and the participation of La-5 aircraft in combat.

The La-5 of the thirty-eighth series or La-5F was a single-engine wooden low-wing aircraft. Like the LaGG-3 and earlier La-5 modifications, the main structural material of the airframe was pine. Delta wood was used for the wing spars and some frames. The wooden parts of the aircraft were glued together. The fuselage consisted of a metal front truss and a wooden monocoque that was made in one piece with the tail. To achieve a certain speed, the sealing of the canopy and the firewall was improved, play and cracks in the ailerons and rudders were eliminated, the external finish was improved, and the number of fuel tanks was reduced to three. The measures taken reduced the weight of the fighter and improved its maneuverability, especially in vertical flight. An important innovation was the installation of a new teardrop-shaped canopy with front and rear armored glass and the possibility of jettisoning the sliding part in case of emergency. Instead of a pneumatic-mechanical trigger, an electric firing mechanism was installed for the cannons: the trigger on the flight stick was replaced by a button. Other external differences include the appearance of two small air intakes in front of the windscreen, which provided the flow of cold air into the cabin.

The time limit of the M-82F engine in take-off mode was removed — essentially the boosted mode of 1,700 hp. became nominal. The armament still consisted of two synchronized 20 mm ShVAK cannons; if necessary, two bomb racks could be installed under the wing to carry 50 or 100 kg bombs.

La-5s played a limited role in the Kuban air battles, as the Red Army Air Forces mainly used other types of fighters there, including Yaks and Airacobras. However, at least one division armed with Lavochkins was transferred to this section of the front at the height of the fighting. The Battle of Kursk was the first major operation in which the La-5F and FN took part: the famous Soviet ace Ivan Kozhedub flew the La-5F. In mid-July, La-5s of the 63rd GIAP arrived from the Kalinin Front, where Alexey Maresyev, who had returned to duty after amputation of both legs, fought and won his first victory.

The La-5F at last had the chance to fight on equal terms with the Bf 109 G-2 and G-4 up to an altitude of 6 km. The vertical maneuvers of the La-5F and the indicated modifications of the Bf 109 were practically the same up to an altitude of 3.5 km; at higher altitudes, the advantage went to the Bf 109. However, by skillfully combining horizontal and vertical maneuvers, the pilot of the La-5F had the initiative in the dogfight up to an altitude of 4 km. Compared to the Fw 190 A-4 and A-5, the La-5F fighter had an advantage in speed and all types of maneuvers at the same altitudes. Thus, the La-5F was not inferior in its main characteristics to the enemy fighters at least in the whole range of altitudes where the air battles were mainly fought on the Eastern Front.

La-5s of the 38th series took part in the battles from 1943 to 1944 when they were gradually replaced by the more advanced La-5FN.

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: 165..183 km/h
Indicated stall speed in takeoff/landing configuration: 147..162 km/h
Dive speed limit: 720 km/h
Maximum load factor: 10 G
Stall angle of attack in flight configuration: 22.7 °
Stall angle of attack in landing configuration: 15.1 °
 
Maximum true air speed at sea level, engine mode - Nominal: 552 km/h
Maximum true air speed at 3000 m, engine mode - Nominal: 580 km/h
Maximum true air speed at 6000 m, engine mode - Nominal: 597 km/h
 
Service ceiling: 10000 m
Climb rate at sea level: 19.5 m/s
Climb rate at 3000 m: 14.4 m/s
Climb rate at 6000 m: 9.5 m/s
 
Maximum performance turn at sea level: 20.8 s, at 300 km/h IAS.
Maximum performance turn at 3000 m: 29.0 s, at 320 km/h IAS.
 
Flight endurance at 3000 m: 1.7 h, at 350 km/h IAS.
 
Takeoff speed: 170..200 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 nominal power.
 
Engine:
Model: M-82F
Maximum power in Nominal mode at sea level: 1700 HP
Maximum power in Nominal mode at 2100 m: 1550 HP
Maximum power in Nominal mode at 5400 m: 1335 HP
 
Engine modes:
Nominal (unlimited time): 2400 RPM, 1140 mm Hg
 
Oil rated temperature in engine output: 55..90 °C
Oil maximum temperature in engine output: 125 °C
Cylinder head rated temperature: 140..210 °C
Cylinder head maximum temperature: 250 °C
 
Supercharger gear shift altitude: 3500 m
 
Empty weight: 2584 kg
Minimum weight (no ammo, 10% fuel): 2844 kg
Standard weight: 3220 kg
Maximum takeoff weight: 3460 kg
Fuel load: 334 kg / 464 l
Useful load: 876 kg
 
Forward-firing armament:
2 x 20mm gun "ShVAK", 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: Summer 1943
 
Operation features:
- The boost regulator on an airplane works only as a boost limiter. The regulator limits the nominal boost to 1140 mmHg at the first stage of the supercharger operation and 950 mmHg at the second stage of the supercharger operation.
- The engine has a two-stage mechanical supercharger which must be manually switched at 3500m altitude.
- Engine mixture control is automatic when the mixture lever is at the rear position. It is possible to manually lean the mixture by moving the lever forward to reduce the 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.
- 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 has trimmers for pitch and yaw controls.
- 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.
- The canopy has an emergency jettison for bailing out at a high speed.
- 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: 100% (auto 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: 100% (auto 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: 5,0 l/min
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