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Motorlet M 701

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Motorlet M-701

The Motorlet M-701 is a Czechoslovakian jet engine. It was used to power the Aero L-29 Delfín jet trainer, with about 9,250 engines built between 1961 and 1989.

Contents

Development and design

In 1955, the Czechoslovakian aero-engine company Motorlet commenced design of a new turbojet engine to power the Aero L-29, a jet trainer being designed by Aero for a competition to equip all Warsaw Pact air forces. The resulting design, designated Motorlet M-701 was a single shaft centrifugal compressor turbojet and was the first jet engine designed in Czechoslovakia (although Motorlet had previously built the Klimov VK-1 under license).

The M-701 was first run in 1958, and engine no.4 was tested on an Avia B-228 flying laboratory in December 1959. Engine no.8 powered the third prototype L-29 when it flew on 12 July 1960 (the first two prototypes had flown the previous year powered by Rolls-Royce Viper engines). The L-29 was selected as the winner of the competition, and was ordered in large numbers, with the M-701 entering production at Jinonice near Prague in 1961. By the time production ended in 1989, more than 9,250 had been built.

Applications

  • Aero L-29 Delfín
  • Specifications

    From: Jane's All the World's Aircraft 1971-72

    General characteristics

  • Type: Single shaft centrifugal flow 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
  • Air mass flow: 19.6 kg/s (37.25 lb/s)
  • Specific fuel consumption: 1.14 (at rated power)
  • Thrust-to-weight ratio: 2.7:1 (0.026 kN/kg)
  • References

    Motorlet M-701 Wikipedia