Jump to content

BMW 018

From Wikipedia, the free encyclopedia

This is an old revision of this page, as edited by 109.152.111.118 (talk) at 17:35, 4 September 2016. The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.

BMW 018
Type Turbojet
Manufacturer BMW
Number built 3

The BMW 018 (RLM designation BMW 109-018) was an early axial-flow turbojet engine project by BMW AG in Germany.[1]

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).[2]

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.[3]

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

Performance

  • Maximum thrust: 34.3 kN (7,700 lbf)

Notes

  1. ^ Christopher, John. The Race for Hitler's X-Planes (The Mill, Gloucestershire: History Press, 2013), p.74.
  2. ^ Christopher, p.74.
  3. ^ Kay, Anthony. German Jet Engine and Gas Turbine Development 1930-1945. 2002, p.131

Sources

  • Christopher, John. The Race for Hitler's X-Planes. The Mill, Gloucestershire: History Press, 2013.
  • Kay, Anthony. German Jet Engine and Gas Turbine Development 1930-1945. 2002