Neha Patil (Editor)

BMW 018

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The BMW 018 (RLM designation BMW 109-018) was an early axial-flow turbojet engine project by BMW AG in Germany.

Contents

The 018 design was begun in 1940. It was generally similar to the 003, but had a twelve-stage axial compressor and three-stage turbine, for a thrust of 34.3 kN (7,700 lbf).

Three engines were at various stages of completion at Staßfurt. It was decided that these examples would be moved to Kolbermoor to finish construction, and then move them to Oberwiesenfeld for testing. Despite this planning, the rapidly deteriorating war situation prompted BMW personnel to destroy the engines and their components in order to prevent them from falling into Allied hands.

Specifications

Data from Christopher, John. The Race for Hitler's X-Planes (The Mill, Gloucestershire: History Press, 2013), p.74.

General characteristics

  • Type: axial flow turbine
  • Length: 4,190 mm (165 in)
  • Diameter: 1,252 mm (49.3 in)
  • Dry weight: 2,295 kg (5,060 lb)
  • Components

  • Compressor: 12-stage
  • Combustors: annular
  • Turbine: 3-stage
  • Performance

  • Maximum thrust: 34.3 kN (7,700 lbf)
  • Power-to-weight ratio:
  • References

    BMW 018 Wikipedia