Jump to content

Motorav 2.6 R

Add links
From Wikipedia, the free encyclopedia

This is the current revision of this page, as edited by Ahunt (talk | contribs) at 01:21, 1 February 2022 (adding templates, removing costing parameters that have been deleted from the template). The present address (URL) is a permanent link to this version.

(diff) ← Previous revision | Latest revision (diff) | Newer revision → (diff)

Motorav 2.6 R
Type Aircraft engine
National origin Brazil
Manufacturer Motorav

The Motorav 2.6 R is a Brazilian aircraft engine, designed and produced by Motorav of Bocaiúva Minas Gerais for use in ultralight and homebuilt aircraft.[1]

Design and development

[edit]

The engine is a four-cylinder four-stroke, horizontally-opposed, 2,600 cc (158.7 cu in) displacement, air-cooled, direct-drive, gasoline engine design. It employs capacitor discharge ignition and produces 95 hp (71 kW) at 2800 rpm.[1]

Specifications (2.6 R)

[edit]

Data from Tacke[1]

General characteristics

  • Type: Four cylinder, four stroke aircraft engine
  • Bore: 94 mm (3.7 in)
  • Stroke: 94 mm (3.7 in)
  • Displacement: 2,600 cc (158.7 cu in)

Components

Performance

  • Power output: 95 hp (71 kW)

See also

[edit]

Related lists

References

[edit]
  1. ^ a b c Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 260-261. Flying Pages Europe SARL, 2015. ISSN 1368-485X
[edit]
Retrieved from "https://en.wikipedia.org/w/index.php?title=Motorav_2.6_R&oldid=1069184168"