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Lyulka AL 21

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Lyulka AL-21

The Lyulka AL-21 is an axial flow turbojet engine created by the Soviet Design Bureau named for its chief designer Arkhip Lyulka.

Contents

Design and development

The AL-21 is similar in power and technology to the General Electric J79 first flown in 1955 which was first engine for supersonic flight using the variable stator. Western analysts believe they were designed by reverse engineering a J-79 engine which was most widely used on the F-4 Phantom from a plane shot down in Vietnam.

After the fall of Soviet Union, it's became clear that AL-21F3 turbojet engine is different and more advanced design than J-79. It sucks in more air, compresses it more, and burns it hotter. AL-21F3 is a later design and superior in all respects. Its compressor is much more advanced getting more compression from less stages. It is generally described as being in the "third generation" of Soviet gas turbine engines which are characterized by high thrust-to-weight ratios and the use of turbine air cooling.


The AL-21 entered service in the early 1960s. With later marks AL-21F3 it was used in the Sukhoi Su-17, Sukhoi Su-24, Ground-attack variant Mikoyan-Gurevich MiG-23, and Sukhoi T-10 (Sukhoi Su-27 prototype). A non-afterburning version powered the Yakovlev Yak-38 VTOL fighter.

General characteristics

  • Type: Afterburning turbojet
  • Length: 5,300 mm (209 in)
  • Diameter: 1,000 mm (39 in)
  • Dry weight: 1,700 kg (3,740 lb)
  • Components

  • Compressor: Two-spool 14-stage axial compressor with variable stator vanes
  • Turbine: Two-stage high pressure, single-stage low pressure
  • Performance

  • Maximum thrust:
  • 76.4 kN (17,175 lbf) dry
  • 109.8 kN (24,675 lbf) with afterburner
  • Overall pressure ratio: 14.75:1
  • Turbine inlet temperature: 1,100 °C (2,000 °F)
  • Specific fuel consumption:
  • 77.5 kg/(h·kN) (0.76 lb/(h·lbf)) at idle
  • 87.7 kg/(h·kN) (0.86 lb/(h·lbf)) at maximum military power
  • 189.7 kg/(h·kN) (1.86 lb/(h·lbf)) with afterburner
  • Thrust-to-weight ratio: 64.7 N/kg (6.6:1)
  • Life expectancy: 1,800 hours
  • References

    Lyulka AL-21 Wikipedia