TWO-BLADED MAIN ROTOR
to be installed on helicopters with up to
50 kg take-off mass and rotor diameter
of 2600 mm (102.36")
OVERVIEW
The state-of-the-art carbon main rotor blades are produced with latest carbon multi- cross-layer technology using a curing oven.
Due to the industrial pro duction process the main rotor blades have long-life endurance, the enhanced aerodynamic performance, the increased wear resistance under severe weather conditions. The blades have superior behavior under extreme maneuvers.
SPECIFICATIONS
Length:
1230 mm
Width:
76-38 mm
Thickness:
12.5-4.5 mm
Root thickness:
12.5 mm
Mounting Hole Size:
6 mm
Rotation:
Left (CCW) or right (CW)
Twist:
10°
Material:
Carbon fiber (prepreg)
Max. RPM:
1300
Weight:
0.42 kg
MTOW (2 blades):
50 kg
