Technical data
Type LM-1
Function observation
Year 1916
Crew 2
Engines 1*150hp Sunbeam
Wingspan 15.10m
Length 10.50m
Wing Area 49.10m2
Empty Weight 1090kg
Loaded Weight1455kg
Wing Load (kg/m2) 29.7
Power Load 9.7
Armament ?

Lebed Morskoj, LM-1

17k LM-1, at "History of aircraft construction in the USSR", Vol.1 p.260

The LM-1 was originally intended for 220hp Renault engine, but was built with much weaker powerplant. Main floats had rubber cord suspension (on rear struts). Third smaller float was attached under the tail.



References:
  • "History of aircraft construction in the USSR", Vol.1 p.260;

  • Created November 25, 1997
    by Alexandre Savine;
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