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Contents

   



(Top)
 


1 Design and development  





2 Specifications (Hirth 3002 E)  



2.1  General characteristics  





2.2  Components  





2.3  Performance  







3 See also  





4 References  














Hirth 3002







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From Wikipedia, the free encyclopedia
 


Hirth 3002
Type Aircraft engine
National origin Germany
Manufacturer Hirth

The Hirth 3002 is a German aircraft engine, that was designed and produced by HirthofBenningen for use in ultralight aircraft.[1]

By March 2018, the engine was no longer advertised on the company website and seems to be out of production.[2]

Design and development

[edit]

The Hirth 3002 is a four-cylinder, two-stroke, horizontally-opposed, 1,042 cc (63.6 cu in) displacement, fan-forced air-cooled, petrol engine design, with a mechanical gearbox reduction drive with reduction ratios from 2.03 to 3.79:1. It employs dual capacitor discharge ignition and produces 83 hp (62 kW) at 6000 rpm.[1]

Specifications (Hirth 3002 E)

[edit]

Data from Tacke[1]

General characteristics

Components

Performance

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 258-259. Flying Pages Europe SARL, 2015. ISSN 1368-485X
  • ^ Hirth. "All Engines". www.hirth-engines.de. Retrieved 19 March 2018.

  • Retrieved from "https://en.wikipedia.org/w/index.php?title=Hirth_3002&oldid=1171035373"

    Categories: 
    Hirth aircraft engines
    Two-stroke aircraft piston engines
    Air-cooled aircraft piston engines
    2000s aircraft piston engines
    Hidden categories: 
    Articles with short description
    Short description matches Wikidata
    Use dmy dates from January 2022
    Use British English from January 2022
     



    This page was last edited on 18 August 2023, at 17:04 (UTC).

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