هلیسا: ظفر ۵۰۰
Helisa: Zafar 500

General data

Producer info

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Names and dates
Market original model designation
ظفر ۵۰۰
Market model designation (english translation or spelling)
Zafar 500
Date of prototype completion
1996
Country of manufacture
Iran
Config info
Rotorcraft typeHelicopter
Weights
Maximum Takeoff Weight (MTOW)
2200
kg
Manufacturers empty weight (MEW)
1200
kg
Cabin and cockpit
Maximum number of people onboard
6
(...)
5
External dimensions
Landing gear type
Skids
Main rotor
Main rotor diameter
11.02
m
Main rotor direction of rotation
Clockwise
Main rotor angular speed
353
rpm
Number of blades
3
Main rotor blade airfoil
NACA 0012
Tail rotor
Tail rotor angular speed
2003
rpm
Number of blades
3
Tail rotor blade airfoil
NACA 0012
Powerplant
Engine model
Artouste IIIB
Engine model (english translation or spelling)
Artouste IIIB
Total maximum power
603
HP
Performance
Max cruise speed
194
km/h
Maximum service ceiling
5486
m
Maximum range
580
km
0.0453