| Technical data |
|---|
| Type |
MR-3bis |
| Function |
Naval Recce |
| Year |
1931 |
| Crew |
2 |
| Engines |
1*500/680hp M-17 |
| Length |
11.4m |
| Wingspan |
15.6m |
| Wing area |
53.0m2 |
| Empty weight |
2050kg |
| Loaded weight |
3100kg |
| Wing Load (kg/m2) |
59.0 |
| Power load (kg/hp) |
6.2 |
| Speed at 0m |
190km/h |
| Landing Speed |
85km/h |
| Landing Roll |
22sec |
| Takeoff Roll |
35sec |
| Range |
720km |
| Flight Endurance |
4h |
| Ceiling |
4000m |
| Armament |
|---|
| Guns |
1...2mg? |
| Bombs |
? |
Biplane flying
boat, development of the MR-3. Hull was redesigned (new shape, wooden
construction). Aircraft was ready in June 30,
1931.
Takeoff shortcomings were cured without changes in flight performance.
There was another variant of the hull built for special high
speed monoplane design (MR-5,
MR-5bis). But more advanced
project MBR-2 was on its final stage,
and MR-5bis was not finished.
| Predecessors | Modifications |
|---|
MR-3 |
None. Dead End. |
