Yak-13 (Yak-12), A.S.YakovlevL ow-wing 3-4 seat liaison monoplane with enclosed cockpit, built in November
1944. Designation Yak-12
fas replaced by Yak-13 after design stage was completed. Yak-13 was equipped by VISh-327
variable-pitch propeller by G.M.Zaslavskij. Construction - mostly wood/plywood, with aluminum skin on tailplane and fin, fabric -
on ailerons and tail controls.
| Technical data | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|
| Type | Yak-13 | |||||||||
| Function | Liaison | |||||||||
| Year | 1945 | |||||||||
| Crew | 1 | |||||||||
| Engines | 1*145hp M-11FM | |||||||||
| Length | 8.45m | |||||||||
| Wingspan | 11.5m | |||||||||
| Wing area | 22.0m2 | |||||||||
| Empty weight | 868kg | |||||||||
| Loaded weight (normal) | 1230kg | |||||||||
| Loaded weight (maximum) | 1310kg | |||||||||
| Wing load | 56kg/m2 | |||||||||
| Power load | 8.5kg/hp | |||||||||
| Speed at 0m | 245km/h | |||||||||
| Landing Speed | 89km/h | |||||||||
| Landing Roll | 375m | |||||||||
| Takeoff Roll | 330m | |||||||||
| Range | 815km | |||||||||
| Flight Endurance | 3.5h | |||||||||
| Ceiling | 4000m | |||||||||
| Climb | ||||||||||
| Rate at 0m | 4.2m/sec | |||||||||
| 1000m | 4.2min | |||||||||
| Payload | ||||||||||
| Fuel | 94+14kg | |||||||||
| Seats | 2-3 | |||||||||
| Created January 25, 1996
Modified February 16, 1999 by Alexandre Savine |
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