Armstrong Siddeley Mongoose
| Mongoose | |
|---|---|
   | |
| Armstrong Siddeley Mongoose fitted to the Shuttleworth Collection's airworthy Hawker Tomtit | |
| Type | Radial engine | 
| National origin | United Kingdom | 
| Manufacturer | Armstrong Siddeley | 
| First run | 1926 | 
| Major applications | Hawker Tomtit Avro 504N  | 
| Developed into | Armstrong Siddeley Serval | 
The Armstrong Siddeley Mongoose is a British five-cylinder radial aero engine produced by Armstrong Siddeley. Developed in the mid-1920s it was used in the Hawker Tomtit trainer and Parnall Peto seaplane amongst others. With a displacement of 540 cubic inches (9 litres) the Mongoose had a maximum power output of 155 horsepower (115 kilowatts).
A Mongoose engine powers the sole remaining airworthy Hawker Tomtit, based at Old Warden.
Design and development
The Mongoose is a five-cylinder, single-row, air-cooled radial piston engine. The engine features twin forward-mounted ignition magnetos and enclosed valve rockers, the cylinders being the same as those used for the earlier Jaguar engine.[1] An unusual feature of the Mongoose is the vertical position of the lower cylinder, a design thought likely to promote oil fouling of the spark plugs.[2]
Built in several variants, power output ranged between 135 and 155 hp (100-115 kW).
Variants
- Mongoose I
 - 1926, 135 hp.
 - Mongoose II
 - 1930, 155 hp.
 - Mongoose III
 - 1929.
 - Mongoose IIIA
 - 1929, civil use.
 - Mongoose IIIC
 - 1929, Military use based on IIIA.
 
Applications
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Note:[3]
- ANBO III (Second batch, 1931)[4]
 - Avro 504N
 - Avro 504R
 - Avro Tutor
 - Avro Type 621 Trainer
 - Handley Page Hamlet
 - Handley Page Gugnunc
 - Hawker Tomtit
 - Parnall Peto
 - Fokker S.IV
 
Surviving engines
An Armstrong Siddeley Mongoose IIIC powers the sole remaining airworthy Hawker Tomtit, K1786/G-AFTA, owned and operated by the Shuttleworth Collection this aircraft flies regularly throughout the summer months.[5]
Specifications (Mongoose I)
General characteristics
- Type: 5-cylinder single-row radial
 - Bore: 5 in (127 mm)
 - Stroke: 5.5 in (139.7 mm)
 - Displacement: 540 cu in (8.8 L)
 - Length: 36.6 in (93 cm)
 - Diameter: 45.6 in (116 cm)
 - Dry weight: 340 lb (154 kg)
 
Components
- Valvetrain: Overhead poppet valves
 - Fuel type: 77 Octane petrol
 - Cooling system: Air-cooled
 - Reduction gear: Direct drive, left-hand tractor
 
Performance
- Power output: 138 hp (103 kW) at 1,750 rpm at sea level
 - Compression ratio: 5:1
 - Power-to-weight ratio: 0.4 hp/lb (0.67 kW/kg)
 
See also
Related development
Comparable engines
Related lists
References
Notes
- ^ Gunston 1989, p. 18.
 - ^ a b Lumsden 2003, p. 69.
 - ^ List from Lumsden
 - ^ Ramoška, Gytis, ANBO III. Pirmasis serijinis lietuviškas lėktuvas, Plieno Sparnai, (in Lithuanian) Nr. 7 2002 m.
 - ^ The Shuttleworth Collection - Hawker Tomtit Archived 10 December 2013 at the Wayback Machine Retrieved: 22 February 2012
 - ^ Lumsden 2003, Part 4.
 
