| Technical data | |
|---|---|
| Type | SAM-5 |
| Function | Passenger |
| Year | 1933 |
| Crew | 1? |
| Engines | 1*100hp M-11 |
| Length | 8.0m |
| Wingspan | 12.5m |
| Wing area | 24.0m2 |
| Empty weight | 626kg |
| Loaded weight | 1106kg |
| Wing Load (kg/m2) | 46.1 |
| Power load (kg/hp) | 11.1 |
| Maximum Speed at 0m | 175km/h |
| Cruise Speed | 140km/h |
| Landing Speed | 71km/h |
| Landing Roll | 180m 20sec |
| Takeoff Roll | 180m 17sec |
| Range | 1760km |
| Ceiling | 3170m |
| Climb | |
| 1000m | 7.5min |
| 2000m | 16.0min |
| 3000m | 30.0min |
| Payload | |
| Seats | 5 |
SAM-5 by A.S.Moskalev
 |
5-seat passenger aircraft, high-wing monoplane of all-metal design. Remarkably light airframe with smooth 0.3mm skin on the fuselage and corrugated (0.3mm also) on the wings. Project approval was not easy - it was hard to convince experts that 5-passenger plane with 100hp engine can boost speed 178km/h and have flight range 1000km. Only positive recommendation of S.P.Korolev (who already was a prominent figure in early 30's) give live to SAM-5.
Aircraft was assembled by workers at Voronezh Aircraft Factory (then still under construction), without sufficient skills and training. As a result, finish quality of the aircraft suffered. Despite of this, performance was very good for aircraft powered with 100hp engine. Large number of flights were performed.
| Predecessors | Modifications |
|---|---|
| - |  SAM-5bis |
| References | Links |
|---|---|
| None found |
