| Technical data | |
|---|---|
| Type | G-21 |
| Function | General |
| Year | 1936 |
| Crew | 1 |
| Engines | 1*150hp M-11E |
| Length | 7.0m |
| Wingspan | 11.0m |
| Wing area | 14.0m2 |
| Empty weight | 705kg |
| Loaded weight | 980kg |
| Wing Load (kg/m2) | 70.0 |
| Power load (kg/hp) | 9.8 |
| Speed at 0m | 220km/h |
| Landing Speed | 70km/h |
| Landing Roll | 85m |
| Takeoff Roll | 80m |
| Range | 500km |
| Flight Endurance | 3h |
| Ceiling | 4760m |
| Climb | |
| 1000m | 5.6min |
| Payload | |
| Fuel+Oil | 105+10kg |
| Seats | 1-2 |
G-21 by V.K.Gribovskij
|
One of first general purpose aircraft built in the USSR. Following roles were suggested for the G-21:
- Tourism
- Sport
- Liaison
- Paramedic
Clean low-wing cantilever monoplane with fixed landing gear and enclosed 2-3 seat cockpit. Leading edge automatic slats were synchronized by steel tube running through the fuselage. Typical for V.K.Gribovskij aircraft stressed skin wooden construction - 2mm plywood monocoque fuselage, wing covered by plywood from the leading edge to the second spar, after the second spar - fabric.
G-21 easily passed all trials, used later for training.
One built.
| Predecessors | Modifications |
|---|---|
| - | - |
| References | Links |
|---|---|
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