The Lavochkin La-11 was designed from the successful Lavochkin La-9 series of piston engine fighters with the difference being that the La-11 was to be a long-range bomber escort. The system was under development in the closing years of World War 2 but was not made ready for service until 1947. In effect, the Lavochkin La-11 became one of the last dedicated piston engine fighters to be produced for the Soviet Air Force and played upon the strengths of the preceding design quite well, though it arrived at a time when the jet age was becoming all the technological rage.
Design of the La-11 followed suit with the preceding La-9 series featuring a stout engine housing with large propeller hub, low monoplane wing assembly and mid-set framed cockpit offering up a decent view with traditional blind spots. Armament consisted of a battery of 3 x 23mm Nudelman-Suranov NS-23 series cannons which were more than capable of engaging enemy aircraft. Power was derived from a single Shvetsov ASh-82FNV radial piston engine producing some 1,870 horsepower and helping the La-11 achieve speeds nearing 420 miles per hour.
The prototype La-11 appeared in two forms as the La-123 and the La-134D. The former was based highly on the La-9 but sported just three cannons as its offensive armament. The latter was an improved La-123 prototype sporting an increased fuel capacity and underwing fuel drop tanks. As the development of the type evolved more and more options related to long-range sorties were introduced to make the pilot's job more comfortable. These options included a more cushioned seat, built-in urine waste facilities, arm and head rests. Communications and navigation equipment were also brought up to modern speed.
At the conclusion of development, it was found that the La-11 was quite a heavier aircraft from the original La-9. This limited the aircrafts combat capabilities above 23,000 feet but still played upon the long-range performance inherent in the new design. Despite this shortcoming, the La-11 was a good performer especially well into missions when fuel consumption would naturally lighten the La-11's load.
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(OPERATORS list includes past, present, and future operators when applicable)
✓Air-to-Air Combat, Fighter
General ability to actively engage other aircraft of similar form and function, typically through guns, missiles, and/or aerial rockets.
Length
28.2 ft (8.60 m)
Width/Span
32.6 ft (9.95 m)
Height
9.7 ft (2.95 m)
Empty Wgt
6,107 lb (2,770 kg)
MTOW
8,807 lb (3,995 kg)
Wgt Diff
+2,701 lb (+1,225 kg)
(Showcased structural values pertain to the base Lavochkin La-11 (Fang) production variant)
Installed:
1 x Shvetsov ASh-82FNV air-cooled radial piston engine developing 1,870 horsepower driving a three-bladed propeller unit at the nose.
(Showcased performance specifications pertain to the base Lavochkin La-11 (Fang) production variant. Performance specifications showcased above are subject to environmental factors as well as aircraft configuration. Estimates are made when Real Data not available. Compare this aircraft entry against any other in our database or View aircraft by powerplant type)
STANDARD:
3 x 23mm Nudelman-Suranov NS-23 cannons.
Supported Types
(Not all ordnance types may be represented in the showcase above)
Hardpoint Mountings: 2
La-134 - Prototype Designation; based on the Lavochkin La-9.
La-134D - Second Prototype Designation; increased fuel and range via improved fuel tank space and underwing fuel tanks.
La-11 - Base Production Fighter Designation
Ribbon graphics not necessarily indicative of actual historical campaign ribbons. Ribbons are clickable to their respective aerial campaigns / operations / aviation periods.
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China; North Korea; Soviet Union
