Stierlin R.

General data

Producer info

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Data sources

Names and dates
Project start date
1967
Date of prototype completion
1969
First flight date and time
1969-05-15
Country of manufacture
Switzerland
People involved
Robert StierlinConstructor
Config info
Rotorcraft typeHelicopter
Config
Single rotor
Way of counteracting main rotor torque
Tail rotor
Weights
Maximum Takeoff Weight (MTOW)
240
kg
Cabin and cockpit
Maximum number of people onboard
2
Cockpit seating arrangement
Side-by-side
Cabin type
Open frame
External dimensions
Landing gear type
Skids
Main rotor
Main rotor equipped with stabilizing bar
Yes
Powerplant
Engine model
Johnson
Engine model (english translation or spelling)
Johnson
Number of engines
1
Total maximum power
88
HP
0.0596