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

22k b/w photo, "History of aircraft construction in the USSR", Vol.1 p.248;

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


  • References:
  • "History of aircraft construction in the USSR", Vol.1 p.248;

  • Modified October 31, 1997 Back to
    Main Gate