Aerospace Engines A to Z
Aerospace Engines A to Z

Updated: 25-Sep-2020

NAEF was an engine builder in Milan. It started in 1909 with a 25/30 CV, water-cooled, inline, four-cylinder engine.

-The same year, another in-line four-cylinder engine came out, with slightly larger cylinder dimensions (140 x 120 mm) and it gave 40/50 CV.

-At the same time the first V8 came out with the same cylinder sizes, and it gave 80 CV.

-The next one and still in 1909, was another larger V8 (170 x 130 mm) that gave 100 CV of power.

-In all models the mentioned power was achieved at 1,200 rpm.

-Later, around 1910, they built an inline 4-cylinder again. This one gave 50/60 CV.

Engines of NAEF (Italy)

Model: 4 cyl. inline, 25/30 HP

Arquitecture: 4-cylinder In-line
Cooling: Liquid
Total Displacement:
Bore / Stroke:
Power: 30 CV @ 1200 rpm
Weight:

Other details:
Model: 4 cyl. inline, 40/50 HP

Arquitecture: 4-cylinder In-line
Cooling: Liquid
Total Displacement:
Bore / Stroke:
Power: 50 CV @ 1200 rpm
Weight:

Other details:
Model: 4 cyl. inline, 50/60 HP

Arquitecture: 4-cylinder In-line
Cooling: Liquid
Total Displacement:
Bore / Stroke:
Power: 60 CV @ 1200 rpm
Weight:

Other details:
Model: V8, 100 HP

Arquitecture: 8-cylinder V-Engine
Cooling: Liquid
Total Displacement:
Bore / Stroke:
Power: 100 CV @ 1200 rpm
Weight:

Other details:
Model: V8, 80 HP

Arquitecture: 8-cylinder V-Engine
Cooling: Liquid
Total Displacement:
Bore / Stroke:
Power: 80 CV @ 1200 rpm
Weight:

Other details: