| Technical data |
| Type |
G-28
|
| Function |
Trainer |
| Year |
1941
|
| Crew |
1 |
| Engines |
1*240hp MV-6
|
| Length |
7.66m |
| Wingspan |
9.0m |
| Wing area |
11.6m2 |
| Empty weight |
897kg |
| Loaded weight |
1157kg |
| Wing Load (kg/m2) |
100 |
| Power load (kg/hp) |
4.8 |
| Speed at 0m |
275km/h |
| Speed at 1600m |
303km/h |
| Landing Speed |
90.5km/h |
| Takeoff Roll |
280m |
| Ceiling |
6600m (calculated) |
| Range |
500km |
| Payload |
| Fuel+Oil |
122+15kg |
Single-seat trainer, transitional to fighter. Trials started in 1941 at NII VVS. G-28 was flown by M.M.Gromov, A.B.Yumashev and P.M.Stefanovskij. When the War broke off, aircraft was evacuated together with NII VVS, and eventually abandoned.
Judgment of the War time took it tall over this good trainer project.
| Predecessors |
Modifications |
| - |
- |
