Stierlin R.: Merlin

General data

Producer info

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Names and dates
Market original model designation
Merlin
Market model designation (english translation or spelling)
Merlin
Also known as
X40
Also known as (english translation or spelling)
X40
Project start date
1952
First flight date and time
1953
Project end date
1958
Country of manufacture
Switzerland
People involved
Robert StierlinConstructor, Test pilot
Roger MercierConstructor, Test pilot
Config info
Rotorcraft typeHelicopter
Weights
Manufacturers empty weight (MEW)
210
kg
Cabin and cockpit
Maximum number of people onboard
1
External dimensions
Length
7.50
m
Height
1.80
m
Main rotor
Main rotor type
Semi-rigit
Main rotor equipped with stabilizing bar
Yes
Main rotor diameter
6.60
m
Main rotor direction of rotation
Counterclockwise
Minimum main rotor angular speed
400
rpm
Maximum main rotor angular speed
450
rpm
Number of blades
2
Main rotor blade airfoil
NACA 23012
Tail rotor
Tail rotor type
Classic tail rotor
Drive type
Drive shaft
Tail rotor diameter
1.20
m
Tail rotor direction of rotation
Counterclockwise
Tail rotor angular speed
1800
rpm
Number of blades
2
Powerplant
Engine model
Salmson
Engine model (english translation or spelling)
Salmson
Engine type
Piston
Total maximum power
45
HP
Angular speed at max power
2200
rpm
Fuel system
Average fuel consumption [volumetric]
16
l/h
Performance
Maximum horizontal flight speed (Vh)
110
km/h
Hover ceiling IGE
2500
m
Hover ceiling OGE
1250
m
Maximum flight endurance
1.25
h
0.1008