AMT NETHERLANDS OLYMPUS Series HP Gas Turbines SKU: AMT-GASTRB-OLMP

AMT NETHERLANDS  designs and manufactures high performance gas turbine engines in different series with different specifications, start system options and delivered thrust ratings.  AMT Olympus Series HP gas turbine engines deliver 230 N at 108.500 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). A spinoff of the Olympus HP is being certified by EASA for the use as a "bringing home device" for a full size glider. For additional information, please refer to the supplied documentation or contact us. 

Mfr. P/N & Title

Volume discounts

Quantity Unit price You Save
3 €5,804.50 Up to €916.50

The Olympus HP (High Performance) Gas Turbine features totally re-designed Compressor, Diffuser and Turbines stages, producing a massive power increase (23,5 Kg / 51.7Lbs ), without reducing the legendary reliability and incredibly fast throttle response of AMT NETHERLANDS  turbines. Like all AMT NETHERLANDS the Olympus HP is available with manual or auto Air-start, as well as fully automatic electric starting.

Product Specifications:

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

Engine diameter 130 mm / 5.1 Inch

Engine length 374 mm / 14.7 Inch

Engine weight 2900 gram / 6.4 Lbs

System airborne weight * 3845 gram / 8,5 Lbs

Thrust at S.T.P. ** 230 N / 51.7 Lbf

Maximum RPM 108.500 / 108.500

Thrust at Idle RPM 13 N / 2.9 Lbf

Pressure ratio 3.8:1 / 3.8:1

Mass flow 450 Gr/sec / 0.99 Lb/Sec

Max continues EGT 750 Deg C / 1380 Deg F

Fuel consumption 640 Gr/min / 22,5 oz/min

Specific fuel consumption 46,4 gr/(Kn*sec) / 1,64 lb/(lbf*hr)

Starting method Direct kerosene starting gas turbine, on request propane start.

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

** On request the RPM can be raised to 110.000 RPM giving 10 Newton additional thrust.

Operating conditions

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

Maximum operating temperature + 50 Deg. Celsius / +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 push button)

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

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

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

AMT-OLMP-AIRST

Data sheet

Certification/Approval
Certificate of Conformance
Taric
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

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