La-5 ser.8 / IL-2 Sturmovik: Great Battles
Close
menu
Fighter
La-5 ser.8
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.

The eighth series La-5 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 were glued together. The fuselage consisted of a metal bulkhead and a wooden monocoque that was integrated with the vertical stabilizer. A design feature of the first series of La-5 was the presence of additional metal-clad formwork from the 5th frame in front of the cabin, which changed the fuselage cross-section from oval to round.

The pilot's cockpit was closed with a sliding canopy that locked in the open and closed positions. On the Series 8 aircraft, poor thermal insulation of the firewall and cabin sides meant that cockpit cooling was still inadequate, allowing heat from the engine and exhaust manifolds to enter the cockpit, resulting in a sharp rise in temperature during flight.

Serial fighters had larger oil coolers than the prototype. A carburetor air intake was installed in the upper part of the engine cowling, and the area of the exhaust manifolds and the cowling above the gun breech increased. From the 8th series aircraft, a complete set of the RSI-4 radio equipment was installed on every second aircraft (this was due to the transition to a new tactical unit — a pair of fighters).

The M-82A engine developed a maximum power of 1700 hp in boosted mode near the ground and 1335 hp at an altitude of 5300 m in nominal mode. The aircraft was armed with 2 synchronized 20 mm ShVAK cannons; if necessary, two bomb racks for carrying bombs of 50 or 100 kg could be installed under the wing.

According to some sources, a total of 200 aircraft of series 2 to 8 were built. Aircraft of the 8th series first appeared at the front in September 1942. The number of La-5s in the Soviet Air Force at the Stalingrad front can be judged from the reports of the 8th Air Army for September-October 1942, which included 18 fighter regiments, of which nine were armed with Yak-1, three with Yak-7, one with Curtiss P-40, one with LaGG-3 and four with La-5. But by the end of the year, the Air Force began to receive enough new vehicles for units armed with the La-5 to change from a rarity to the rule. The pilots of the 5th Guards Fighter Regiment noted: "In air battles with fascist planes, the La-5 proved to be exceptionally good. It is easy to fly, stable and durable".

Despite its good flight characteristics, the La-5 had many defects that had not been eliminated, and most importantly, "the pilots were tormented by the African heat in the cockpit, and the soles of the sergeants' boots were burned and cracked after ten flights."

The La-5 participated in combat from August 1942 until the summer of 1943, when it was replaced by more advanced variants.

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 - Boosted: 550 km/h
Maximum true air speed at 3000 m, engine mode - Boosted: 575 km/h
Maximum true air speed at 6200 m, engine mode - Nominal: 595 km/h
 
Service ceiling: 9700 m
Climb rate at sea level: 19 m/s
Climb rate at 3000 m: 14.0 m/s
Climb rate at 6000 m: 8.8 m/s
 
Maximum performance turn at sea level: 21.7 s, at 290 km/h IAS.
Maximum performance turn at 3000 m: 32.0 s, at 300 km/h IAS.
 
Flight endurance at 3000 m: 1.9 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 Boosted power.
 
Engine:
Model: M-82
Maximum power in Boosted mode at sea level: 1700 HP
Maximum power in Nominal mode at sea level: 1400 HP
Maximum power in Nominal mode at 2100 m: 1550 HP
Maximum power in Nominal mode at 5300 m: 1335 HP
 
Engine modes:
Nominal (unlimited time): 2400 RPM, 950 mm Hg
Boosted power (up to 5 minutes): 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: 2648 kg
Minimum weight (no ammo, 10% fuel): 2928 kg
Standard weight: 3353 kg
Maximum takeoff weight: 3593 kg
Fuel load: 370 kg / 521 l
Useful load: 945 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: September 1942
 
Operation features:
- The engine has a boost mode. To set boost mode it is necessary to push the boost knob and increase manifold pressure to 1140 mm Hg.
- The boost control is effectively a limiter. It limits the pressure to 950 mm Hg in normal mode and to 1140 mm Hg in the boost mode.
- 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 set to maximum. It is possible to manually lean the mixture by moving the mixture control to less than maximum. This also reduces 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 all flight-controls: pitch, roll and yaw.
- 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.
- Cockpit canopy has a weak lock when in the opened position, for this reason the canopy may spontaneously close in a deep dive. 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: auto mixture control
- recommended position of the cowls flap control handles: open
- recommended position of the oil radiator flap control handle: close
- recommended position of the prop pitch control handle: 100%
- recommended position of the throttle lever: 5%
 
2. Recommended mixture control lever positions for various flight modes: 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: 9.7 l/min
- Combat engine mode: 11.1 l/min
Up