Revmaster R-2100D
| {{Infobox Aircraft Begin
| name=R-2100D | image= | caption= }}{{Infobox Aircraft Engine |type=Horizontally opposed piston engine |manufacturer=Revmaster |designer=Joe Horvath |national origin= |first run= |major applications= |produced= |number built= |program cost= |unit cost=$1,095 in 1971 |developed from=Volkswagen air-cooled engine |variants with their own articles= }} |
The Revmaster 2100D is a Volkswagen air-cooled engine modified for homebuilt aircraft with dual magneto ignition.{{cite journal|journal=Air Trails|date=Winter 1971|page=85}}{{cite journal|journal=Sport Aviation|date=September 1977|page=21}}{{cite journal|journal=Sport Aviation|title=The Maloof Controllable Propeller|date=January 1978}}
Specifications (variant)
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|type=
|ref=
|bore=92
|stroke=78
|displacement=2073cc
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|valvetrain=Single overhead exhaust valve, single side inlet valve per cylinder
|supercharger=
|turbocharger=
|fuelsystem=Single carburettor
|fueltype=
|oilsystem=
|coolingsystem=Air-cooled
|power=65hp
|specpower=
|compression=
|fuelcon=
|specfuelcon=
|oilcon=
|power/weight=
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|reduction_gear=
|general_other=
|components_other=Tillotson Floatless Carburetor
|performance_other=
}}
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References
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