| Technical data | |
|---|---|
| Type | M-12 |
| Function | fighter |
| Year | 1916 |
| Crew | 1 |
| Engines | 1*110hp Le Rhone |
| Wingspan | 8.75m |
| Length | 7.60m |
| Wing Area | 26.00m2 |
| Empty Weight | 620kg |
| Maximum Weight | 870kg |
| Wing Load (kg/m2) | 33.5 |
| Power Load | 8.0 |
| Speed at 0m | 140km/h |
| Duration | 2.7 hrs |
| Ceiling | 4000m |
| Climb | |
| 1000m | 6.0min |
| 2000m | 12.0min |
| Armament | |
| Guns | 1*mg 7.62mm, fixed in nose |
M-12, D.P.Grigorovich/ S.S.Schetinin
|
Development of the M-11. The hull was redesigned to improve its hydrodynamics, and the structure was made lighter. Performance was substantially improved (handling and climb).
Only a few were built, and were used in combat during the civil war.
| Predecessor(s): | Modification(s): |
 M-11 |
- |
More Links...
- M-12
- M-12, Grigorovich
- "History of aircraft construction in the USSR", Vol.1 p.248;
References:
