Hirth HM 515

Last updated
Hirth HM 515
Type Inline piston engine
National originGermany
Manufacturer Hirth-Motoren GmbH, Stuttgart-Zuffenhausen
Major applications Siebel Si 202C Hummel
Developed from Hirth HM 500

The Hirth HM 515 was a four-cylinder air-cooled inverted inline engine, intended to power light aircraft of the 1940s. Due to World War II, demand for the light aircraft to be powered by the HM 515 dried up and only the Siebel Si 202C Hummel was powered by development engines before further work was abandoned.

Contents

The HM 515 closely followed the Hirth formula of Elektron (magnesium alloy) castings for the crank case and covers, with roller bearings and metered oil feeds for light weight, smooth running and low oil consumption. Only a small number were produced before the war precluded further production of the light aircraft class that the engine was intended to power. Flight testing was carried out in the Si 202Cs driving a 1.8 m (5 ft 11 in) propeller, but no production ensued. [1]

Specifications (HM 515)

Data from Flugzeug-Typenbuch. Handbuch der deutschen Luftfahrt- und Zubehör-Industrie 1944 [2]

General characteristics

74 kg (163 lb) wet, equipped

Components

Performance

  • 65 PS (64 hp; 48 kW) at 2,100 rpm for take-off
  • 60 PS (59 hp; 44 kW) at 2,040 rpm (high power rating) at sea level
  • 55 PS (54 hp; 40 kW) at 1,990 rpm (max. continuous) at sea level

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References

  1. "Siebel Si 202 Hummel". www.histaviation.com. Retrieved 4 February 2020.
  2. Schneider, Helmut (Dipl.Ing.) (1944). Flugzeug-Typenbuch. Handbuch der deutschen Luftfahrt- und Zubehör-Industrie 1944 (in German) (Facsimile reprint 1986 ed.). Leipzig: Herm. Beyer Verlag. p. 396. ISBN   381120484X.

Further reading