Microjet Engineering

Turbine Technology

The design for the Turbo-Prop has been based on the standard HF65, 100 and 150 engine units and at present can provide up to 130 horsepower.

Based on the weight of an 82 kilo piston engine of comparable power, the Turbo-Prop is an incredible 7 times lighter.

This weight advantage, combined with its multi-fuel facility, results in greater economy and a much higher power to weight ratio.

The design has many other benefits over the equivalent piston engine, some are listed below:-

Extended service intervals based on the greater structural integrity of the engine design,

Direct airframe mounting,

Greatly reduced vibration,

Flexible prop size,

Reduction in engine noise,

Engine upgrades to achieve greater horsepower.

The Turbo-Prop is versatile in its application:-

Generators,

Experimental aviation aircraft,

UAV/Drones and small missiles,

Helicopters,

Gliders.

The possibilities are endless!

For more information on Microjet products, please email Sarah Ford.

E.C.U.

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Webmistress: Gloria Ford
Page created: 5th February 2004
Last modified: 8th December 2004
E&OE