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Armstrong Siddeley Double Mamba
1940s British turboprop aircraft engine
1940s British turboprop aircraft engine
| Field | Value |
|---|---|
| name | Double Mamba |
| image | File:ASDoubleMamba.JPG |
| caption | Preserved Double Mamba at the Imperial War Museum Duxford |
| engine_type | Turboprop |
| manufacturer | Armstrong Siddeley |
| first_run | 29 September 1949 (First flight) |
| major_applications | Fairey Gannet |
| developed_from | Armstrong Siddeley Mamba |
The Armstrong Siddeley Double Mamba is a turboprop engine design developed in the late 1940s of around 3000-4000 hp. It was used mostly on the Fairey Gannet anti-submarine aircraft developed for the Fleet Air Arm of the Royal Navy.
Design and development
The Double Mamba (rarely known as the Twin Mamba) was a development of the Armstrong Siddeley Mamba with two Mambas driving contra-rotating propellers through a combining gearbox.
Engine starting was by cartridge; forced air restart was possible in flight. One engine could be shut down in flight to conserve fuel. Shutting down one engine also stopped one of the propellers.
Variants

;ASMD.1:2,950 shp (2 x ASMa.3) used on Fairey Gannet A.S. Mk.1 and Blackburn B-88 ;ASMD.3:3145 shp (2 x ASMa.5) used on Fairey Gannet A.S. Mk.4 ;ASMD.4:3875 hp (2 x ASMa.6) used on Fairey Gannet AEW Mk.3 ;ASMD.8:3875 hp (2 x ASMa.6) used on Fairey Gannet AEW Mk.3
Applications
- Blackburn B-88
- Fairey Gannet
- Fairey Gannet AEW The Double Mamba engine was also proposed for the Westland Westminster, a 30-seat helicopter that was later built as a prototype powered by a pair of Napier Eland E220 turboshaft engines.
Engines on display
Preserved Double Mamba engines are on public display at the:
- Australian National Aviation Museum
- Deutsches Museum Flugwerft Schleissheim
- Gatwick Aviation Museum
- South Yorkshire Aircraft Museum
- Imperial War Museum Duxford
- Midland Air Museum
- Queensland Air Museum
- East Midlands Aeropark
- Museum of Berkshire Aviation
Specifications (ASMD.3)
|url-status=dead |archive-url=https://web.archive.org/web/20110520160325/https://www.flightglobal.com/pdfarchive/view/1954/1954%20-%200979.html |archive-date=20 May 2011 |power/weight=1.36 eshp/lb |thrust/weight=
References
Notes
Bibliography
- Gunston, Bill. World Encyclopedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989.
References
- Gunston 1989, p.20.
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