Technical data
Type 3-EA
Function experimental
Year 1933
Crew 1
Engines 2*120hp M-2
Rotor diameter 11.0m
Empty weight 982kg
Flight weight 1145kg

3-EA, TsAGI/ A.M.Cheremukhin

Had some construction improvements compared with 1-EA. Tested only 'on the rope', no free flights.

One built.

PredecessorModifications

1-EA

5-EA

Sources [6], Vol.2 p.416;

Modified March 24, 1997 Back to
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