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Motorlet M701C-500 Turbojet

I decided it was time to buy a really big engine :)


The Motorlet engine being hoisted





General characteristics



  • Type: Single shaft centrifugal turbojet engine
  • Length: 2,067 mm (81.38 in)
  • Diameter: 896 mm (35.28 in) (Max width): Max height 928 mm (36.53 in)
  • Dry weight: 330 kg (728 lb)

Components



  • Compressor: Single-stage centrifugal
  • Combustors: 7 straight flow combustion chambers
  • Turbine: Single-stage axial-flow with 61 blades

Performance



  • Maximum Thrust: 8.75 kN (1,962 lbf) (Take-off power -15,500 rpm), 7.87 kN (1,764 lbf) (Rated power - 14,950 rpm)
  • Overall Pressure Ratio: 4.3:1
  • Specific Fuel Consumption: 1.14 (at rated power)


And it came out of this exact aircraft (G-ODAT), A Czechoslovakian L-29 'Delfin' jet trainer:


L29 Delfin

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