AMT Pegasus Gas Turbine
  • AMT Pegasus 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 Pegasus Series HP gas turbine engines deliver 167 N at 119.500 RPM. They are offered in E-start or AIR start (10-12 Bar) configuration, with propane start or kerosene start system. For additional information, please refer to the supplied documentation or contact us. 

Mfr. P/N & Title

Volume discounts

Quantity Unit price You Save
3 €4,372.04 Up to €690.32

Pegasus HP Gas Turbine is a completely  new high performance version of AMT NETHERLANDS original Pegasus turbine engine.  With an astonishing 16-17  kg thrust at 119.500 RPM, this new engine is a fully redeveloped version featuring, in addition to  a 25%  increase in thrust,  reduced fuel consumption, much improved throttle-response, faster start-up's and lower EGT's. The redesign includes many new parts, including the main shaft, bearings,turbine wheel, combustion chamber, turbine stator (NGV), and higher specification of fuel pump. The new motor also includes a smart anodised inlet and front cap, and Festo quick-connectors to make installation easier.

The new Pegasus HP  comes in two versions with an Air Start or Electric Start system and a full 2 year warranty.

Engine set includes: AMT engine, ECU, pump, battery, thermo sensor, mounting straps.

Pegasus HP gas-turbine Specifications:

E-start system / Air-start system

Diameter: 120 mm / 120 mm

Length: 342 mm / 264 mm

Turbine Weight: 2255 gram / 2125 gram

System Weight *: 3075 gram / 2705 gram

Thrust @ max. rpm: 167 N / 167 N

Thrust @ min. rpm: 6 N / 6 N

Maximum RPM: 119,500 / 119,500

Idle RPM: 37,000 / 37,000

Pressure ratio @ max. rpm: 3,2 :1 / 3,2 :1

Mass flow @ max. rpm: 375 gr/sec. / 375 gr/sec.

Normal EGT: 600 C / 600 C

Maximum EGT: 675 C / 675 C

Fuel consumption @ max. rpm: 485 gr/min. / 485 gr/min.

Fuel: JP-4/petroleum/Jet A1

Oil 4,5% aeroshell 500 mixed with fuel

* System airborne weight. (complete system): engine, ECU, pump, battery, thermo sensor, mounting straps.


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