وزارت سپاه: ظفر ۲۰۰
Ministry of Revolutionary Guards: Zafar 300

General data

Producer info

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Names and dates
Market original model designation
ظفر ۲۰۰
Market model designation (english translation or spelling)
Zafar 300
Also known as
سید الشهدا ظفر ۲۰۰
Also known as (english translation or spelling)
Seyedo Shohada Zafar 300
Project start date
1987-03-20
First flight date and time
1989-01-31
Country of manufacture
Iran
People involved
Akbar Akhundzadeh {اکبر آخوند زاده}Chief design engineer
Seyyed Tadin {سيد تدين}Test pilot
Config info
Rotorcraft typeHelicopter
Config
Single rotor
Way of counteracting main rotor torque
Tail rotor
Weights
Maximum Takeoff Weight (MTOW)
1300
kg
Manufacturers empty weight (MEW)
758
kg
Cabin and cockpit
Maximum number of people onboard
2
Cockpit seating arrangement
Tandem
External dimensions
Fuselage width
0.78
m
Total length (rotors turning)
12.08
m
Overal height
2.92
m
Landing gear type
Skids
Main rotor
Main rotor diameter
10.77
m
Tail rotor
Tail rotor diameter
1.58
m
Powerplant
Engine model
Allison 250-C18
Engine model (english translation or spelling)
Allison 250-C18
Engine type
Turboshaft
Number of engines
1
Total maximum power
317
HP
Fuel system
Fuel tank capacity
270
l
Performance
Never exceed speed (Vne)
241
km/h
Maximum flight endurance
3
h
0.0347