| 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 (kg/m2) | 56 |
| Power load (kg/hp) | 8.5 |
| 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 |
Yak-13 (Yak-12), A.S.Yakovlev
|
Low-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 designed by G.M.Zaslavskij. Construction - mostly wood/plywood, with aluminum skin on tailplane and fin, fabric - on ailerons and tail controls.
Aluminum landing flaps installed under the fuselage and wing roots. Main landing gear - retractable, tailwheel - fixed.
Trials took place in 1945. Performance was found good, but contemporary high-wing Yak-10 was found more promising. Yak-13 was abandoned.
| Predecessors | Modifications |
|---|---|
 Yak-5 |
... |
| References | Links |
|---|---|
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