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

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, 1,186 cc (72.4 cu in) 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 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

  • Type: Four cylinder, four stroke aircraft engine
  • Bore: 80 mm (3.1 in)
  • Stroke: 59 mm (2.3 in)
  • Displacement: 1,186 cc (72.4 cu in)
  • Length: 585 mm (23.0 in)
  • Width: 485 mm (19.1 in)
  • Height: 565 mm (22.2 in)
  • Dry weight: 84 kg (185.2 lb)

Components

Performance

See also

Related lists

References

  1. 1 2 3 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. 1 2 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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