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BMW 6012

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This is an old revision of this page, as edited by Nimbus227 (talk | contribs) at 16:42, 19 January 2021 (Undid revision 1001417826 by Norcalangela (talk) See MOS:TENSE). The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.

6012
BMW 6012 engine on display at the Deutsches Museum
Type Turboshaft
National origin Germany
Manufacturer BMW
First run c.Template:Avyear
Major applications Dornier Do 32

The BMW 6012 (later MTU 6012) was a German turboshaft and gas generator engine. Designed in the late-1950s by BMW the engine powered the Dornier Do 32 helicopter and was also used as an auxiliary power unit (APU).

Applications

Specifications

Data from Deutsches Museum.[2]

General characteristics

  • Type: Turboshaft
  • Length:
  • Diameter:
  • Dry weight:

Components

Performance

  • Maximum power output: 80 kW (107 shp)

See also

Comparable engines

Related lists

References

Wikimedia Commons has media related to BMW 6012.
Notes
  1. ^ www.deutsches-museum.de - Dornier Do 32 Retrieved: 18 January 2021
  2. ^ www.deutsches-museum.de - BMW 6012A Retrieved: 18 January 2021
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