VIJA J-10Si explained

The VIJA J-10Si is a French aircraft engine, designed and produced by VIJA Aircraft Engines of Toulouse for use in ultralight and homebuilt aircraft.[1]

The company was founded in 2004 and went out of business in about 2015, ending production.[2] [3]

Design and development

The engine is a four-cylinder four-stroke, in-line, 11861NaN1 displacement, 16 valve, air-cooled, fuel injected motorcycle conversion, petrol engine design, with a mechanical gearbox reduction drive with a reduction ratio of 2.55:1. It employs electronic ignition and produces 1000NaN0 at 6600 rpm, with a compression ratio of 10.5.[1]

Variants

J-10Si
  • Base model with a weight of 841NaN1.[4]
    J-10Sbi
  • Model with a weight of 791NaN1.[4]

    External links

    Notes and References

    1. Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 262-263. Flying Pages Europe SARL, 2015.
    2. Web site: Moteur Vija J-12Si . ulmag.fr . 25 April 2018.
    3. Web site: VIJA-Engines . Internet Archive Wayback Machine . 25 April 2018.
    4. Web site: Produits. 15 April 2018. VIJA Aircraft Engines. vija-engines.com. 25 April 2018. https://web.archive.org/web/20130102052119/http://vija-engines.com/images/2010/Produits-2010.html. 2 January 2013. live. dmy-all.

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