Свербиль В. А.: СВ-3
Sverbil V. A.: SV-3

General data

Producer info

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Names and dates
Market original model designation
СВ-3
Market model designation (english translation or spelling)
SV-3
Project start date
1990
(...)
1991
Date of prototype completion
1996
First flight date and time
1996
Country of manufacture
Russia
People involved
Vasily Sverbil {Василий Свербиль}Constructor
Config info
Rotorcraft typeHelicopter
Config
Single rotor
Way of counteracting main rotor torque
Tail rotor
Weights
Maximum Takeoff Weight (MTOW)
1500
kg
Manufacturers empty weight (MEW)
950
kg
Cabin and cockpit
Maximum number of people onboard
2
Cockpit seating arrangement
Side-by-side
External dimensions
Length
9.22
m
Width
3.65
m
Height
3.80
m
Wheelbase
2.95
m
Main landing gear wheel diameter
0.50
m
Main landing gear wheel width
0.15
m
Nose landing gear wheel diameter
0.30
m
Nose landing gear wheel width
0.13
m
Main rotor
Main rotor diameter
13
m
Main rotor direction of rotation
Clockwise
Main rotor angular speed
300
rpm
Longitudinal rotor axis tilt
4.50
°
Number of blades
3
Tail rotor
Tail rotor type
Classic tail rotor
Tail rotor diameter
2.06
m
Tail rotor direction of rotation
Counterclockwise
Tail rotor angular speed
1450
rpm
Number of blades
2
Powerplant
Engine model
M-14 P {М-14 П}
Engine type
Piston
Number of engines
1
Total maximum power
360
HP
Fuel system
Fuel type
No translation available for: ai-93
Fuel tank capacity
200
l
Average fuel consumption [volumetric]
65
l/h
Performance
Maximum horizontal flight speed (Vh)
150
km/h
Cruise speed (Vc)
130
km/h
Maximum service ceiling
4500
m
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