Porsche 005
| 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
[edit]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
[edit]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
- Compressor: Axial flow
Performance
- Maximum thrust: 500 kg (1,102 lb) static
- Overall pressure ratio: 2.8:1
- Thrust-to-weight ratio: 2.5
References
[edit]- ^ Pocock, Rowland (1967). German Guided Missiles of the Second World War. Arco Publishing Company. p. 24.
- ^ a b Zaloga, Steven (2005). V1 Flying Bomb 1942-1952. Osprey. p. 64. ISBN 9781841767918.
- ^ 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.
- ^ 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).