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Porsche 005

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Porsche 005
Type Turbojet
National origin Germany
Design group Porsche KG
Major applications V-1 flying bomb (planned)
Status Unbuilt design

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

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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 240 km (149 mi) to 700 km (435 mi) 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

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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]

General characteristics

  • Type: Turbojet
  • Length: 2,850 mm (112 in)
  • Diameter: 650 mm (25.6 in)
  • Dry weight: 200 kg (441 lb) for complete power unit

Components

Performance

References

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