| Technical data | |
|---|---|
| Type | La-160 |
| Function | Fighter |
| Year | 1947 |
| Crew | 1 |
| Engines | 1*900/1350kg RD-10F |
| Length | 10.06m |
| Wingspan | 8.95m |
| Wing area | 15.9m2 |
| Empty weight | 2738kg |
| Loaded weight | 4060kg |
| Wing Load (kg/m2) | 255 |
| Power load (kg/hp) | 0.333 |
| Speed at 5700m | 1050km/h |
| Range | 500km |
| Armament | |
| Guns | 2*37mm cannons N-37 |
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The first Soviet swept-wing fighter, development of the La-152. Thin wing with 35° leading edge had same installation as on the La-152, tailplane was slightly raised. On the design stage extensive wind tunnel studies were performed at TsAGI.
Flight trials in June-September 1947 provided designers with reliable data on stability and handling of swept-wing aircraft. Necessity of upper-wing fences at subsonic and supersonic speed was revealed. Such fences were installed, two on each wing.
La-160 carried much more fuel (1080l) than predecessors and pair of powerful cannons. Its engine could gain extra 50% of thrust using improved afterburner (by I.A.Merkulov) on same RD-10F engine. But aircraft was still too small to have sufficient range and carry large weapon load. All possible was taken from the engine design, and the La-160 became the last Soviet fighter to be powered with engine of the RD-10 line.
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| Predecessors | Modifications |
|---|---|
| La-152 |
![]() La-168 |
| References | Links |
|---|---|
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| Created January 25, 1996 Modified February 03, 1998 |
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