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).

6012
BMW 6012 engine on display at the Deutsches Museum
Type	Turboshaft
National origin	Germany
Manufacturer	BMW
First run	c.1960
Major applications	Dornier Do 32

Applications

• Dornier Do 32[1]
• Dornier Do 32K

Specifications

Data from Deutsches Museum.[2]

General characteristics

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

Components

• Compressor:
• Fuel type: Jet fuel

Performance

• Maximum power output: 80 kW (107 shp)
• Power-to-weight ratio:

See also

Comparable engines

• Turbomeca Palouste

Related lists

• List of aircraft engines

References

Wikimedia Commons has media related to BMW 6012.

Notes

This aircraft engine article is missing some (or all) of its specifications. If you have a source, you can help Wikipedia by adding them.

На других языках

[it] BMW 6012 L