| Technical data | ||
|---|---|---|
| Type | La-5FN | |
| Function | Fighter Prototype | Series Fighter |
| Year | 1943 | |
| Crew | 1 | |
| Engine | ASh-82FN | |
| Takeoff Power | 1850hp | |
| Power at 1550m | 1630hp | |
| Power at 4500m | 1500hp | |
| Length | 8.60m | |
| Height | ?m | |
| Wingspan | 9.80m | |
| Wing area | 17.50m2 | |
| Empty weight | 2706kg | 2828kg |
| Loaded weight | 3168kg | 3290kg |
| Wing Load (kg/m2) | 181 | 188 |
| Power load (kg/hp) | 2.17 | 2.25 |
| Speed at altitude | ||
| 0m (boosted) | 593km/h | 583km/h |
| 6250m | 648km/h | 634km/h |
| Landing | 137km/h | 138km/h |
| Landing Roll | ?m | ?m |
| Takeoff Roll | ?m | ?m |
| Turn time | 18.5sec | 18.5sec |
| Range | ?km | ?km |
| Flight Endurance | ?h | ?h |
| Ceiling | 11200m | 10750m |
| Climb | ||
| 5000m | 4.7min | 5.2min |
| Payload | ||
| Fuel+Oil | 345+50kg | |
| Armament | ||
| Guns | 2*20mm ShVAK | |
| Bombs | 4*50kg | |
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During offensive stage of the Battle for Stalingrad new Lavochkin aircraft made its debut. In Summer 1943 the La-5FN in substantial numbers, making massive show during the Kursk Bend battle. While the La-5 was even with most of German front line fighters at low/medium altitudes, it still had some shortage in climb. With new 'Lavochkin' arrival this gap was filled.
Externally La-5FN differed from the late production La-5 by more articulated air intake on the top of the engine cowling, providing more room (and more air) demanded by new ASh-82FN supercharged engine with direct fuel injection. Fairings on the cooling/exhaust side louvers were removed. Slightly larger new VISh-105V (3m diameter) propeller was installed.
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But 'hidden' changes were even more substantial. More powerful engine with better altitude performance was supplemented by airframe improvements. Those included new suction operated leading edge slats and radically improved balance of controls (following the TsAGI expertise). As a result, La-5FN and later aircraft of this line became the most lightly controlled fighters of their time. In addition, large ailerons provided it with excellent roll characteristics.
Improvements in wing structure allowed to use larger fuel tanks, but this opportunity was realised only on few batches. Commonly, tanks volume as same or even smaller than on the La-5.
La-5 pilots complains about excessive cockpit heat were taken into account, and La-5FN provided sufficient comfort. Spartan cockpit instrumentation was absolutely sufficient for daylight prop fighter.
In effort to improve high altitude performance of the La-5FN small batch of La-5FN-TK was built. Those fighters were equipped with turbo-chargers designed by Treskin. Quite commonly, marginal high altitude advantages were outweighted by performance losses at low and medium altitudes - where 'Lavochkins' were mostly used. High altitude fighter on Eastern front was not a pressing priority, and this project was abandoned.
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Drawing from Watson's Military, used to produce a background for this page; |
| Predecessors | Modifications | ||
|---|---|---|---|
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La-5 |
La-7 |
LA-5FN-TK | |
![]() La-5 '206' |
VI | ||
| References | Links | |
|---|---|---|
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| Created January 25, 1996 Modified October 07, 1999 |
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