Lavochkin La-11

The Lavochkin La-11 (NATO reporting name Fang) was an early post-World War II long-range piston-engined Soviet fighter aircraft.

Development

One of the recommendations from the government testing of Lavochkin La-130 (Lavochkin La-9 prototype) was to further develop it into a long-range escort fighter. The resultant La-134 prototype (also sometimes referred to as La-9M) featured increased fuel and oil capacity. Armament was reduced to three cannons. The prototype flew in May 1947. The second prototype, La-134D had fuel capacity increased by an additional 275 liters (73 US gallons) with wing and external fuel tanks. The aircraft was fitted with larger tires to accommodate the increased weight and amenities for long flights such as increased padding in the seat, armrests, and a urinal. In addition, a full radio navigation suite was installed. Not surprisingly, combat performance with a full fuel load suffered. However, as the fuel load approached that of La-9, so did the performance. The aircraft was found to be poorly suited for combat above 7,000 m (23,000 ft). The new fighter, designated La-11 entered production in 1947. By the end of production in 1951, a total of 1,182 aircraft were built.

Operational history

First documented combat use of La-11 took place on April 8, 1950, when these fighters shot down an American Consolidated PB4Y-2 Privateer over the Baltic Sea with all 10 crew lost. Later the same year, La-11 shot down a Lockheed P2V Neptune. By July 1950, La-11 were flying combat air patrol missions over North Korea. The aircraft's main target during the Korean War was the Douglas A-26 Invader night bomber, although numerous skirmishes with North American P-51 Mustangs also took place. Attempts to intercept Boeing B-29 Superfortress bombers proved fruitless. La-11 required 26 minutes to reach B-29's cruise altitude and once there had a speed advantage of only 20 km/h (12 mph) making it easy for the B-29 to evade the attacker in a shallow dive.

Users

• Template:USSR
• Template:PRC
• Template:PRK

Specifications (La-11)

General characteristics

• Crew: One
• Length: 8.62 m (28 ft 3 in)
• Wingspan: 9.80 m (32 ft 2 in)
• Height: 3.47 m (11 ft 5 in)
• Wing area: 17.6 m² (189 ft²)
• Empty weight: 2,770 kg (6,107 lb)
• Loaded weight: 3,730 kg (8,223 lb)
• Max takeoff weight: 3,996 kg (8,810 lb)
• Powerplant: 1× Shvetsov ASh-82FN air-cooled radial engine with a two-stage supercharger and fuel injection, 1,380 kW (1,850 hp)

Performance

• Maximum speed: 674 km/h (420 mph) at altitude
• Range: 2,235 km (1,393 mi)
• Service ceiling: 10,250 m (33,620 ft)
• Rate of climb: 758 m/min (2,486 ft/min)
• Wing loading: 212 kg/m² (44 lb/ft²)
• Power/mass: 0.37 kW/kg (0.23 hp/lb)

Armament

• 3x 23 mm Nudelman-Suranov NS-23 cannons, 75 rounds/gun

References

Notes

Biblliography

• Gordon, Yefim. Lavochkin's Piston-Engined Fighters (Red Star Volume 10). Earl Shilton, Leicester, UK: Midland Publishing Ltd., 2003. ISBN 1-85780-151-2.
• Kopenhagen, W (ed.), Das große Flugzeug-Typenbuch (in German). Transpress, 1987, ISBN 3-344-00162-0

External links

• http://www.aviation.ru/La/#11

See also

Related development

• La-126
• La-138
• La-9

Comparable aircraft
P-51 Mustang Designation sequence

• VVS sequence: La-5 - La-7 - La-9 - La-11 - La-15
• Lavochkin prototypes sequence: La-126 - La-130 - La-132 - La-134 - La-138 - La-140 - La-150

Related lists

• List of fighter aircraft

The initial version of this article was based on material from aviation.ru. It has been released under the GFDL by the copyright holder.

This article is licensed under the GNU Free Documentation License. It uses material from the Wikipedia article "Lavochkin La-11".