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LOM M132





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The LOM M132 is a Czech aircraft engine, designed and produced by LOM Praha (Letecke Opravny Malesice, Praha) of Prague for use in light aircraft.[1]

Type Aircraft engine
National origin Czech Republic
Manufacturer LOM Praha s.p.

Design and development

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The engine is a four-cylinder four-stroke, in-line, 3,980 cc (242.9 cu in) displacement, air-cooled, direct drive gasoline engine design. It employs dual magneto ignition and produces 90 kW (121 hp) for take-off at 2700 rpm, with a compression ratio of 6.3.[1][2]

Variants

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M132A
Model for limited aerobatics, to a maximum of 5 seconds inverted flight.[1][2]
M132AK
Model for advanced aerobatics, including inverted flight.[1][2]

Applications

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Specifications (M132A)

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Data from Tacke and manufacturer[1][2]

General characteristics

Components

Performance

See also

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Related development

Related lists

References

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  1. ^ a b c d e Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 258-259. Flying Pages Europe SARL, 2015. ISSN 1368-485X
  • ^ a b c d LOM Praha. "M132A / M132AK". www.pistovemotory.cz. Retrieved 19 March 2018.
  • ^ Gordon, Yefim; Komissarov, Sergey (2013). Unflown Wings: Soviet and Russian Unrealised Aircraft Projects 1925-2010. Manchester: Créey Publishing. p. 472.
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    Retrieved from "https://en.wikipedia.org/w/index.php?title=LOM_M132&oldid=1229687482"
     



    Last edited on 18 June 2024, at 05:14  





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    This page was last edited on 18 June 2024, at 05:14 (UTC).

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