Simonini Victor 2 Plus

{{Short description|Italian aircraft engine}}

{{Use dmy dates|date=January 2022}}

{{Use British English|date=January 2022}}

{{Infobox Aircraft Begin

| name=Victor 2 Plus

| image=

| caption=

}}{{Infobox Aircraft Engine

|type=Aircraft engine

|manufacturer=Simonini Racing

|designer=

|national origin=Italy

|first run=

|major applications=

|produced=

|number built=

|developed from=

|variants with their own articles=

}}

The Simonini Victor 2 Plus is an Italian aircraft engine, designed and produced by Simonini Racing of San Dalmazio di Serramazzoni for use in ultralight aircraft.Bertrand, Noel; Rene Coulon; et al: World Directory of Leisure Aviation 2003-04, pages 220-221. Pagefast Ltd, Lancaster UK, 2003. {{ISSN|1368-485X}}

Design and development

The Victor 2 Plus is a twin in-line cylinder two-stroke, liquid-cooled, petrol engine design, with a mechanical gearbox reduction drive with reduction ratios of 2.76:1 to 4.00:1. It employs dual capacitor discharge ignition and produces {{convert|102|hp|kW|0|abbr=on}} at 6200 rpm.

Very similar to the Simonini Victor 2 Super, the Victor 2 Plus uses a bore that is {{convert|2|mm|in|2|abbr=on}} smaller and this results in a displacement that is {{convert|38|cc|cuin|1|abbr=on}} smaller.

Specifications (Victor 2 Plus)

{{pistonspecs|

|ref=World Directory of Leisure Aviation 2003-04

|type=Twin cylinder, two stroke aircraft engine

|bore={{convert|80|mm|in|1|abbr=on}}

|stroke={{convert|76|mm|in|1|abbr=on}}

|displacement={{convert|764|cc|cuin|1|abbr=on}}

|length={{convert|648|mm|in|1|abbr=on}}

|diameter=

|width={{convert|410|mm|in|1|abbr=on}}

|height={{convert|490|mm|in|1|abbr=on}}

|weight={{convert|52|kg|lb|1|abbr=on}}

|valvetrain=

|supercharger=

|turbocharger=

|fuelsystem=

|fueltype=petrol

|oilsystem=

|coolingsystem=liquid

|power={{convert|102|hp|kW|0|abbr=on}} at 6200 rpm

|specpower=

|compression=9.5:1

|fuelcon=

|specfuelcon=

|oilcon=

|power/weight=

|designer=

|reduction_gear=mechanical gearbox reduction drive, reduction ratios of 2.76:1 to 4.00:1

|general_other=

|components_other=

|performance_other=

}}

See also

{{aircontent

|see also=

|related=

|similar aircraft=

|lists= *List of aircraft engines

}}

References

{{Reflist}}