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Kuznetsov NK-87

The Kuznetsov NK-87 is a low-bypass turbofan engine rated at 127.5 kN[1] (28,700 lbf) thrust. It powers the Lun-class ekranoplan. It is made by the soviet Kuznetsov Design Bureau (now JSC Kuznetsov).

NK-87
Type Turbofan
National origin Soviet Union
Manufacturer Kuznetsov Design Bureau
First run January 1983[1]
Major applications Lun-class ekranoplan
Spasatel
Developed from NK-86

Applications

Specifications (NK-87)

Data from Otechestvennaya aviatsionno-kosmicheskaya tekhnika - SAMARSKIY NTK[1]

General characteristics

  • Type: Two-spool low-bypass afterburning turbofan
  • Length:
  • Diameter: 1,455 mm (57.3 in)[1] in compressor
  • Dry weight: 2,200 kg (4,900 lb)[1]

Components

  • Compressor:

Performance

See also

Comparable engines

Related lists

References

  1. ^ a b c d e f g h i j Otechestvennaya aviatsionno-kosmicheskaya tekhnika - SAMARSKIY NTK (in Russian). Samara, Russia: SNTK imeni N.D.Kuznetsova. pp. 41, 77.

kuznetsov, bypass, turbofan, engine, rated, thrust, powers, class, ekranoplan, made, soviet, kuznetsov, design, bureau, kuznetsov, 87type, turbofannational, origin, soviet, unionmanufacturer, kuznetsov, design, bureaufirst, january, 1983, major, applications, . The Kuznetsov NK 87 is a low bypass turbofan engine rated at 127 5 kN 1 28 700 lbf thrust It powers the Lun class ekranoplan It is made by the soviet Kuznetsov Design Bureau now JSC Kuznetsov NK 87Type TurbofanNational origin Soviet UnionManufacturer Kuznetsov Design BureauFirst run January 1983 1 Major applications Lun class ekranoplan SpasatelDeveloped from NK 86 Contents 1 Applications 2 Specifications NK 87 2 1 General characteristics 2 2 Components 2 3 Performance 3 See also 4 ReferencesApplications EditLun class ekranoplan Spasatel proposed Specifications NK 87 EditData from Otechestvennaya aviatsionno kosmicheskaya tekhnika SAMARSKIY NTK 1 General characteristics Type Two spool low bypass afterburning turbofan Length Diameter 1 455 mm 57 3 in 1 in compressor Dry weight 2 200 kg 4 900 lb 1 Components Compressor Performance Maximum thrust 127 5 kN 28 700 lbf 1 at takeoff Overall pressure ratio 13 1 Bypass ratio 1 17 1 Turbine inlet temperature 1 280 K 1 010 C 1 840 F 1 Specific fuel consumption 54 kg kN h 1 at takeoff Power to weight ratio See also EditComparable engines Kuznetsov NK 86Related lists List of aircraft enginesReferences Edit a b c d e f g h i j Otechestvennaya aviatsionno kosmicheskaya tekhnika SAMARSKIY NTK in Russian Samara Russia SNTK imeni N D Kuznetsova pp 41 77 This aircraft engine article is missing some or all of its specifications If you have a source you can help Wikipedia by adding them Retrieved from https en wikipedia org w index php title Kuznetsov NK 87 amp oldid 1050287101, wikipedia, wiki, book, books, library,

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