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AMT Titan

2007 : The Titan has been constructed from a single radial compressor and an axial flow turbine stage.

Copyright text and pictures AMT Netherlands

The time required for the Titan to spool up and down is also positively influenced by the low mass of the axial turbine wheel, taking less than 4 seconds from min. to max. rpm and only 3 seconds from max. rpm to min. rpm.

The combustion chamber is of the annular type, which is fitted with a unique "low pressure" fuel system. Both the front and the rear hybrid bearings are lubricated and cooled by the fuel system, and therefore the motor requires no separate lubrication system or oil tank.

The turbine is protected from misuse and accidental damage by means of a microprocessor based controller (ECU) which regulates operation of the engine within pre programmed software limits. The ECU is fully automatic and needs no adjustment by the operator.


Engine diameter 147 mm / 5.8 Inch
Engine length 385 mm / 15.1 Inch
Engine weight 3645 gram / 8.0 Lbs
System airborne weight * 5211 gram / 11,5 Lbs
Thrust at S.T.P. at max RPM 392 N / 88.2 Lbf
Maximum RPM 96.000 / 96.000
Thrust at Idle RPM 13 N / 2.9 Lbf
Pressure ratio at max RPM 3.8:1 / 3.8:1
Mass flow 660 Gr/sec / 1.46 Lb/Sec
Max continues EGT 850 Deg C / 1562 Deg F
Fuel consumption 1020 Gr/min / 36 oz/min
Specific fuel consumption 43.3 gr/(Kn*sec) / 1,53 lb/(lbf*hr)

Starting method Direct kerosene starting gasturbine, on request propane start.

* Total weight of; Engine,ECU,pump,battery,thermosensor, valves, mounting straps.