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Jacobs R-830

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Template:Infobox Aircraft Engine

The Jacobs R-830 or L-5 is a seven-cylinder, air-cooled, radial engine for aircraft manufactured in the United States, production started in 1935.[1]

Design and development

The R-830 was effectively an enlargement of the R-755 with strengthened stressed parts. With a bore and stroke of 5.0 in × 5.5 in (140 mm × 127 mm) the displacement was 831 cu in (13.6 L), takeoff power was around 285 hp (212 kW). The engine features steel cylinders with aluminum-alloy cylinder heads.

Applications

Specifications (L-5)

Template:Pistonspecs

See also

Related development

Related lists

References

Notes

  1. Gunston 1989, p.85.

Bibliography

  • Gunston, Bill. World Encyclopedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. ISBN 1-85260-163-9

External links

Template:Jacobs aeroengines Template:US military piston aeroengines

This article is licensed under the GNU Free Documentation License.
It uses material from the Wikipedia article "Jacobs R-830".