Porsche 005 Explained

The Porsche 005 (full RLM designation 109-005) was a small, single-use turbojet design intended to power a long-range version of the V-1 flying bomb.[1] [2] [3] At the end of World War II, the design of the Porsche 005 turbojet had not been finalised and no parts had been constructed.[3]

Design and development

The Argus As 014 pulsejet used in production V-1 flying bombs was simple to build but relatively fuel inefficient. Design of the Porsche 005 began in late 1944 with the aim of providing a more fuel efficient engine for the V-1 allowing for greater ranges. The use of the Porsche 005 turbojet was projected to increase the range of the V-1 from 240abbr=onNaNabbr=on to 700abbr=onNaNabbr=on and allow launching without ramps.[3]

During the last months of World War II the Porsche 005 project was being led by Dr Max Adolf Mueller,[3] who had worked on jet engine projects for both Junkers and Heinkel.[3] [4] Dr Mueller was taken into captivity at the end of the war, and later prepared a drawing of the Porsche 005 for American investigators. Post-war, Porsche did not continue work on gas turbines or jet engines.[3]

Specifications

Note that only limited progress on the Porsche 005 design had been made by the end of World War II.[2] [3] Known engine data and targeted performance is shown:[3]

Notes and References

  1. Book: Pocock, Rowland. German Guided Missiles of the Second World War. 1967. Arco Publishing Company. 24. en.
  2. Book: Zaloga, Steven . V1 Flying Bomb 1942-1952 . 2005 . Osprey. en. 9781841767918. 64.
  3. Book: Kay, Antony L . German Jet Engine and Gas Turbine Development 1930-1945. 2002 . Airlife Publishing Ltd . en. 9781840372946. 153-155.
  4. Meher-Homji . Cyrus B . Prisell . Erik. American Society of Mechancial Engineers (ASME) . Pioneering Turbojet Developments of Dr. Hans Von Ohain from the HeS 1 to the HeS 011. International Gas Turbine & Aeroengine Congress & Exhibition. Indianapolis, Indiana. 7–10 June 1999.