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"PROTOR" 2-seat helicopter

Performance&Specifications Sheet

Main rotor diameter, m 9.00
Tail rotor diameter 1.56
Main rotor RPM 384
Tail rotor RPM 2206
V cruise, kmh 140
V max, kmh 165
Endurance, hours 3.0
Rate of climb, m/sec 4.0
Autorotation best rate of descent, m/sec 6.0
Service ceiling, m 3000
Range, normal, km 400
Engine VAZ-413 VAZ-416
Horsepower 152 170
Engine RPM 6000 6000
Take-off weight, kg 800 830
MTOW, kg 830 890
Useful load, kg 300 330
Fuel autogaz autogaz
Fuel capacity, litres 110 130

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This page was published on Sept.19, 2001

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