|
|
Purpose:
Gas turbine turboshaft aero engine
Description:
Designed to power updated Mi-2M helicopter and multipurpose
helicopters. It is passing special bench and
certification tests.
Technical details:
|
Takeoff (SLS, ISA, oinlM 1.0):
|
|
|
power, hp
|
400
|
|
specific fuel consumption, kg/h/hp
|
0.28
|
|
Max cruise (SLS, ISA, Оіпід 1.0):
|
|
|
power, hp
|
285
|
|
specific fuel consumption, kg/h/hp
|
0.32
|
|
Dimensions, mm
|
1 047 x 538 x 684
|
|
Weight, dry (according to GOST17106-79), kg
|
115
|
|
