Mirocopter: SCH-2A

General data

Producer info

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Names and dates
Market original model designation
SCH-2A
Market model designation (english translation or spelling)
SCH-2A
Project unveiling date
2019-01-15
Country of manufacture
Slovenia
People involved
Miro Crv {Miro Črv}Constructor
Config info
Rotorcraft typeHelicopter
Config
Coaxial rotors
Weights
Maximum Takeoff Weight (MTOW)
250
kg
Manufacturers empty weight (MEW)
113
kg
Cabin and cockpit
Maximum number of people onboard
1
Cabin type
Open frame
External dimensions
Fuselage length
3
m
Length
4.37
m
Width
1.50
m
Height
2.45
m
Landing gear width
1.50
m
Control system
Lateral control
Main rotor
Longitudinal control
Main rotor
Yaw control
Rudder
Main rotor
Main rotor type
Flapping blades
Main rotor diameter
4.37
m
Main rotor direction of rotation (System no.: 1)
Counterclockwise
Main rotor direction of rotation (System no.: 2)
Clockwise
Number of blades (System no.: 1)
2
Number of blades (System no.: 2)
2
Main rotor blade airfoil
NACA 0012 (mod)
(...)
NACA 8H12
Main rotor mass
4
kg
Powerplant
Engine model
Fiate MZ202
(...)
Hirth
Engine model (english translation or spelling)
Fiate MZ202
(...)
Hirth
Engine type
Piston
Engine dry weight
30
kg
Number of engines
1
Total maximum power
60
HP
Angular speed at max power
5800
rpm
Fuel system
Fuel tank capacity
19
l
Average fuel consumption [volumetric]
17
l/h
Performance
Maximum horizontal flight speed (Vh)
100
km/h
Cruise speed (Vc)
80
km/h
Maximum flight endurance
1
h
0.096