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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]

J-10Si
Type Aircraft engine
National origin France
Manufacturer VIJA Aircraft Engines

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, 1,186 cc (72.4 cu in) displacement, 16 valve, air-cooled, fuel injected motorcycle conversion, gasoline engine design, with a mechanical gearbox reduction drive with a reduction ratio of 2.55:1. It employs electronic ignition and produces 100 hp (75 kW) at 6600 rpm, with a compression ratio of 10.5.[1]


Variants


J-10Si
Base model with a weight of 84 kg (185.2 lb).[4]
J-10Sbi
Model with a weight of 79 kg (174.2 lb).[4]

Specifications (J-10Si)


Data from Tacke[1]

General characteristics

Components

Performance


See also


Related lists


References


  1. Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 262-263. Flying Pages Europe SARL, 2015. ISSN 1368-485X
  2. "Moteur Vija J-12Si". ulmag.fr. Retrieved 25 April 2018.
  3. "VIJA-Engines". Internet Archive Wayback Machine. Retrieved 25 April 2018.
  4. VIJA Aircraft Engines (25 April 2018). "Produits". vija-engines.com. Archived from the original on 2 January 2013. Retrieved 15 April 2018.





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