Agusta_GA.40 Knowpia

Agusta GA.40
Type	2-cylinder, air-cooled, horizontally opposed aircraft engine
National origin	Italy
Manufacturer	Agusta
Designer	M. Ginnini
First run	1955

The Agusta GA.40 was a 2-cylinder, air-cooled, horizontally opposed engine developed in Italy by Agusta for light aircraft use. It was intended for use in motorgliders. The engine was produced in the 1950s and 1960s.^[1]

Specifications edit

Data from Jane's All the World's Aircraft 1962-63^[2]

General characteristics

Type: 2-cylinder air-cooled horizontally opposed aircraft piston engine
Bore: 100 mm (3.94 in)
Stroke: 95 mm (3.74 in)
Displacement: 1.492 L (91.05 in³)
Length: 613 mm (24.13 in)
Width: 785 mm (30.91 in)
Height: 450 mm (17.72 in)
Dry weight: 56 kg (123 lb) dry
Designer: M. Ginnini

Components

Valvetrain: pushrod operated overhead valve, 1x inlet + 1x exhaust per cylinder
Fuel system: Stromberg NAS 3A1 carburettor
Fuel type: 80/87 octane
Oil system: Pressure lubrication with a gear driven pump
Cooling system: Air-cooled

Performance

Power output: 31.32 kW (42 hp) at 2,700rpm
Specific power: 20.99 kW/L (0.46 hp/in³)
Power-to-weight ratio: 0.559 kW/kg (0.34 hp/lb)

Applications edit

Corby Starlet
Kokkola Ko-04

Notes edit

^ "none". Flight. July 1957.
^ Taylor, John W.R. FRHistS. ARAeS (1962). Jane's All the World's Aircraft 1962-63. London: Sampson, Low, Marston & Co Ltd.