| Technical data |
| Type |
G-10
|
| Function |
Sport |
| Year |
1933
|
| Crew |
1 |
| Powerplant (1) |
| Type |
M-23
|
Walter |
| Power |
65hp |
60hp |
| Size (m) |
| Length |
5.6 |
| Wingspan |
8.4 |
| Wing area |
11.0m2 |
| Weights (kg) and Loads |
| Empty |
335 |
330 |
| Loaded |
510 |
505 |
| Wing Load (kg/m2) |
46.4 |
45.8 |
| Power load (kg/hp) |
7.8 |
8.4 |
| Speed (km/h) |
| at 0m |
170 |
165 |
| Landing |
67 |
67 |
| Roll (m) |
| Takeoff |
80 |
| Landing |
100 |
| Ceiling (m) |
| Maximum |
5200 |
4800 |
| Climb (min) |
| 1000m |
5.0 |
5.5 |
| 2000m |
11.0 |
13.0 |
| 3000m |
20.0 |
23.0 |
| Range (km) |
| Practical |
700 |
| Flight Endurance |
4h |
| Payload |
| Fuel+Oil |
75+10kg |
High-wing sport monoplane. Wing was installed on central pylon and V-struts. Fuselage - monocoque of very elegant shape. Clean design allowed to get exceptional performance with engines used.
The G-10 was built in 1931 at GAZ-1.
During light aircraft contest (1935 or 1936, Tushino) G-10 was flown by young pilot N.Fedoseev. 34 aircraft took off for 5000km race Moscow - Gorky - Kazan - Sarapul - Perm - Sverdlovsk - Chelabinsk - Magnitogorsk - Kujbyshev - Saratov - Lugansk - Donetsk - Dnepropetrovsk - Kiev - Briansk - Moscow. First place was taken by A.S.Yakovlev AIR-10, G-10 finished second.
| Predecessors |
Modifications |
| - |
- |
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