Searchable Light Aviation Database

Marcmotor Ros 200

Specifications:

Power: 40 hp / 9000 rpm
Displacement: 196 cc
Weight: 35 lbs (16 kg)
Cycles: Two cycle
Cylinders configuration: 2 inline
Fuel: Gasoline
Cooling: Air fan
Propeller drive: Mechanical redrive
Marcmotor Ros 200

Ros 200`s description

type of engine two stroke, two cylinders
displacement 196,34 cc
stroke 50 mm
bore 50 mm
cooling forced air
ignition cdi system charging battery 12v
power 40 hp at 9000 rpm
max rpm 9500 rpm
muffler different types of exhaust
weight 15,8 kg
clutch ---------------
starter recoil and electric start
reduction gear ratio 3,5 : 1
carburetor two walbro
cylinder al-nicasil
Compression 10,6 : 1

Description from the website http://www.marcmotor.com/sito/eng/marc_d.htm on 2014-05-18.

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