AMT Titan Gas Turbine
  • AMT Titan Gas Turbine


AMT NETHERLANDS  designs and manufactures high performance gas turbine engines in different series with different specifications, start system options and delivered thrust ratings.  AMT TITAN Series gas turbine engines deliver 392 N at 96.000 RPM. They are offered in E-start or AIR start (10-12 Bar) configuration, with propane start or kerosene start system and with or without the Engine Data Terminal (EDT). For additional information, please refer to the supplied documentation or contact us. 

Mfr. P/N & Title

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Titan gas turbine owes much of its excellent performance and superb power/weight ratio to a new design diffuser stage. This revolutionary type of diffuser also allows the relative small engine diameter. 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 and from min. to max. rpm and only 3 seconds from max. rpm to min. rpm. Like all AMT turbines, the Titan  is available with manual or auto Air-start, as well as fully automatic electric starting.  

Each Titan turbine set contains the folowing parts.

1 x Fully tested Titan E-start gasturbine with kerosene start system (Thrust 392 Newton at STP.)

1 x Version 2.0 b Electronic Control Unit.

1 x High flow main solenoide valve for kerosene.

1 x High flow fuel solenoide valve for ignitor.

1 x Titan fuel pump.

1 x Rear engine mount.

1 x Front engine mount + EGT sensor mount.

1 x 4 cell 3300Mah Lithium Polymer battery pack.

1 x Battery pack charge cable.

1 x Safety clip for RPM sensor.

1 x Thermo sensor (K-type).

1 x Manual Titan E-start.

1 x 3 meter Festo PP3 tube.

1 x 2 meter Festo PP4 tube.

1 x 2 meter Festo PP6 tube.

1 x Fuel filter.

1 x Festo T piece for ignitor feed.

1 x Engine Data Terminal (optional).

1 x EDT charge cable

Product Specifications:

(All data at STP +/- 2%, S.T.P. : 15 Degrees Celsius / 59 Degrees Fahrenheit, Pressure : 1013 Mbar / 29.91 in)

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.

Operating conditions

Min operation temperature * - 25 Deg. Celcius / -13 Deg F

Maximum operating temperature + 50 Deg. Celcius / +122 Deg F

Maximum operating altitude 8000 Meter / 26250 feet

Maximum operating speed 1000 Km / hour / 620 Mile / hour

* With the use of LiPo batteries the minimum operation temperature is limited to -10 Deg Celsius.

Engine control possibilities

1 x RS232 Throttle and switch settings including special functions *

2 x PWM between 1-2 milliseconds ** Throttle and switch settings. (special functions * with puch button)

2 x Analog inputs 0-5 volt DC ** Throttle and switch settings. (special functions * with puch button)

* Activation of prime function, igniter function, starter function, speed cool.

** Specify ECU at ordering with PWM inputs or Analog inputs.


Data sheet

Certificate of Conformance
8411110010 Turbojets of thrust below 25 kN
Unit of Measurement (UOM) / Sale
Each (ea.)
Common Procurement Vocabulary (CPV) Code
34731100-1 Aircraft engines

Specific References