| Technical data |
|---|
| Type |
Guep-1 |
| Function |
trainer |
| Year |
1933 |
| Crew |
2 |
| Engines |
1*100hp M-11 |
| Length |
?m |
| Height |
?m |
| Wingspan |
?m |
| Wing area |
?m2 |
| Empty weight |
615kg |
| Loaded weight |
880kg |
| Wing Load (kg/m2) |
? |
| Power load (kg/hp) |
8.8 |
| Speed at 0m |
160km/h |
| Landing Speed |
70km/h |
| Landing Roll |
120m 10sec |
| Takeoff Roll |
100m 10sec |
| Range |
500km |
| Flight Endurance |
3.0h |
| Ceiling |
3500m |
| Climb |
| 1000m |
8min |
| 2000m |
18min |
| 3000m |
36min |
| Payload |
|---|
| Fuel+Oil |
190kg |
Guep-1 by Friedrich Guep
German
designer Friedrich Guep was invited in
1932
to work within the GVF system. He brought with him a project
of light aircraft, which was built in very short time at ZOK
NII GVF.
Guep-1 was a monoplane of mixed construction. Fuselage had wielded steel tube frame,
strut-braced wooden wing had constant chord. All skin - fabric.
Aircraft was used as a trainer for several years since
1933.
It was very stable and had good handling.
| Predecessors | Modifications |
|---|
| - |
- |
