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Soviet Lavochkin LaGG-3 fighter1,2,3,4

Lavochkin LaGG-3 fighter, captured by the Finns:
Soviet Lavochkin LaGG-3 fighter

Lavochkin LaGG-3-2 VRD, fighter:
Soviet Lavochkin LaGG-3 fighter

Design

Designed by Semyon Lavochkin, V. Gorbunov, and M. Gudkov.1,3,4

The LaGG-3 and LaGG-1 were produced primarily out of wood.1,2,3,4 The control surfaces were light alloy with a fabric cover.1,2,3 Flaps were all metal to be as strong as possible.1

LaGG-1 Deficiencies

Pilots complained that the controls felt heavy and didn't climb very well.3

Engine

There engine was started by a Hucks starter.1 The propeller was constant speed.2,3 The liquid cooled engine lead to difficulties maintaining it in the field.2

Wing

The wing had birch plywood skinning that was impregnated and bonded with phenolformaldehyde resin.1

Cockpit

The cockpit didn't have a very good view for the pilot.1

Tail wheel

The tail wheel was retractable.4

Prototype

The I-22 prototype first flew on March 30, 19391,2,3 / March 30, 19404.

The LaGG-1 was found to have handling and performance problems.4

The LaGG-1 prototype, the I-22, was modified as the I-301 which lead to the LaGG-3.1,3

The I-301 prototype first flew on June 14, 1940.4

Production

The LaGG-1 started production in 1940.3 Production of the LaGG-3 ended in June 1942.4

Variants

Usage

Invasion of the Soviet Union

Two regiments had the LaGG-1.3 There were 300 LaGG-3s available in June 1941.1

Escorts

The LaGG-3s were relegated to being escorts for the Ilyushin Il-2s.3

Captured by Finland

At least two were captured and used by Finland.1

Captured by Japan

The Japanese had at least one LaGG-3.1

  Lavochkin LaGG-11,2,3 Lavochkin LaGG-31,2,3,4
Type   Fighter1,2,3,4
Crew   11,2,3
Engine (Type) Klimov M1052,3,4 Klimov M-105PF-11
Klimov M-105PF piston2,3,4
Cylinders V 123 V 121,3,4
Inline2
Cooling   Liquid1
HP 1,0503, 1,1004 1,2401,2,3,4
Propeller blades   31,4
Fuel capacity    
Dimensions    
Span   32' 1.75"2,3, 32' 2"1,4
9.8 m1,2,3,4
Length   28' 11"3, 29' 1.25"2, 29' 2"1, 29' 2.5"4
8.81 m3, 8.87 m2, 8.9 m1,4
Height   8' 10"2,3,4, 14' 5"1
2.69 m4, 2.7 m2,3, 3.3 m1
Wing area   188 ft2 1, 188.4 ft2 2, 188.5 ft2 3
17.5 m2 1,2, 17.51 m2 3
Weight    
Empty   5,776 lb1,3,4
2,620 kg1,3,4
Loaded   7,231 lb1,4, 7,275 lb3
3,280 kg1,4, 3,300 kg3
Performance    
Speed 373 mph2, 376 mph3
600 kph2, 605 kph3
 
Speed at sea level   307 mph4
494 kph4
Speed @ 11,975' /
3,650 m
  348 mph2
560 kph2
Speed @ 16,400' /
5,000 m
  348 mph1
560 kph1
Speed @ 16,405' /
5,000 m
  348 mph4, 357 mph3
560 kph4, 575 kph3
Climb   2,950'/minute2,3,4
900 m/minute2,3,4
Climb to 16,400' /
5,000 m
  5.85 minutes1
Climb to 16,405' /
5,000 m
  5.9 minutes4
Service ceiling   29,530'2, 31,495'4, 31,500'1, 31,825'3
9,000 m2, 9,600 m1,4, 9,700 m3
Range   404 miles1,2,3
650 km1,2,3
Armament 1: 20 mm2,3
2: 12.7 mm2,3
2: 12.7 mm UBS2,3
2: 7.62 ShKAS MG2,3
Propeller hub   1: 20 mm4
1: 20 mm ShVAK1,2,3
120 rounds1
OR   1: 23 mm4
Above engine   2: 12.7 mm4
2: 12.7 mm BS1
220 rounds each1
OR   2: 7.62 mm MG4
Rockets   6: 3.23"2,3
6: 82 mm1,2,3,4
OR    
Bombs - under wings   441 lb4
2: 220 lb1
4: 110 lb2,3
200 kg4
2: 100 kg1
4: 50 kg2,3

Sources:

  1. Aircraft of WWII, General Editor: Jim Winchester, 2004
  2. Fighting Aircraft of World War II, Editor: Karen Leverington, 1995
  3. The Encyclopedia of Weapons of World War II, General Editor Chris Bishop, 1998
  4. Aircraft of WWII, Stewart Wilson, 1998
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