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Tumansky RD-9

The Tumansky RD-9 (initially designated Mikulin AM-5) was an early Soviet turbojet engine, not based on pre-existing German or British designs. The AM-5, developed by scaling down the AM-3,[1] was available in 1952 and completed testing in 1953; it produced 25.5 kN (5,700 lbf) thrust without afterburner. The AM-5 engine is notable for making possible the first mass-produced supersonic interceptors such as the MiG-19, and the first Soviet all-weather area interceptor, the Yak-25.[2] When Sergei Tumansky replaced Alexander Mikulin as the OKB-24's chief designer in 1956, the engine was renamed RD-9.[citation needed] The engine was later built under license in China as the WP-6.

RD-9
Preserved Tumansky RD-9B turbojet engine
Type Turbojet
Manufacturer Tumansky
First run 1953
Major applications Yak-25
MiG-19

Variants and applications edit

 
A BAF FT-6's Wopen WP-6A turbojet engines on display at Bangabandhu Military Museum, Bangladesh
RD-9A
RD-9B
Used in the East German civilian jetliner project Baade 152 in 1958 and 1959, replaced when Pirna 014 engines became available.
RD-9AK
Non-afterburning versions for the Yak-25 and Yak-26.
RD-9AF-300
Afterburning version for the Yak-27 and Yak-28.
RD-9AF2-300
Afterburning version for the Yak-27 and Yak-28.
RD-9B
Afterburning version for the early variants of MiG-19.
RD-9BK
Version for Lavochkin La-17M.
RD-9BF-811
Afterburning version for the later variants of MiG-19.
RD-9V
Afterburning version used in the Ilyushin Il-40P.
WP-6
Chinese built version for the Shenyang J-6.
WP-6A
a Chinese upgraded version for the Nanchang Q-5 and J-6C.
WP-6Z
further developed for the cancelled Nanchang J-12
NK-TJ
[i] North Korean version built for MiG-19 and Shenyang J-6[3]

Specifications (RD-9BF-811) edit

Data from [4][5]

General characteristics

  • Type: Afterburning turbojet
  • Length: 5,560 mm (219 in)
  • Diameter: 668 mm (26 in)
  • Dry weight: 725 kg (1,600 lb)

Components

Performance

  • Maximum thrust: 3,000 kgf (6,600 lbf, 29 kN) military power, 3,750 kgf (8,300 lbf, 37 kN) with afterburner
  • Turbine inlet temperature: 860 °C
  • Specific fuel consumption: 0.96 lb/(lbf⋅h) or 27 g/(kN⋅s) military power / 1.6 lb/(lbf⋅h) or 45 g/(kN⋅s) afterburner

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See also edit

Comparable engines

Related lists

Notes edit

  1. ^ designation is just a placeholder

References edit

  1. ^ Belyakov, R.A.; Marmain, J. (1991). MiG 1939-1989. Paris: Editions Larivière. p. 137. ISBN 2-907051-00-8.
  2. ^ Leonard, Barry (January 2011). History of Strategic and Ballistic Missile Defense: Volume II. DIANE Publishing. p. 245. ISBN 9781437921311.
  3. ^ "북한의 무인기 Mm-1".
  4. ^ "Mikulin AM-5 / Tumansky RD-9 / Wopen WP-6".
  5. ^ "Турбореактивный двигатель РД-9".
  • The Osprey Encyclopedia of Russian Aircraft: 1875-1995, Bill Gunston, ISBN 1-85532-405-9.

External links edit

  • RD-9B page on LeteckeMotory.cz (cs)

tumansky, initially, designated, mikulin, early, soviet, turbojet, engine, based, existing, german, british, designs, developed, scaling, down, available, 1952, completed, testing, 1953, produced, thrust, without, afterburner, engine, notable, making, possible. The Tumansky RD 9 initially designated Mikulin AM 5 was an early Soviet turbojet engine not based on pre existing German or British designs The AM 5 developed by scaling down the AM 3 1 was available in 1952 and completed testing in 1953 it produced 25 5 kN 5 700 lbf thrust without afterburner The AM 5 engine is notable for making possible the first mass produced supersonic interceptors such as the MiG 19 and the first Soviet all weather area interceptor the Yak 25 2 When Sergei Tumansky replaced Alexander Mikulin as the OKB 24 s chief designer in 1956 the engine was renamed RD 9 citation needed The engine was later built under license in China as the WP 6 RD 9Preserved Tumansky RD 9B turbojet engineType TurbojetManufacturer TumanskyFirst run 1953Major applications Yak 25MiG 19 Contents 1 Variants and applications 2 Specifications RD 9BF 811 2 1 General characteristics 2 2 Components 2 3 Performance 3 See also 4 Notes 5 References 6 External linksVariants and applications edit nbsp A BAF FT 6 s Wopen WP 6A turbojet engines on display at Bangabandhu Military Museum BangladeshRD 9A RD 9B Used in the East German civilian jetliner project Baade 152 in 1958 and 1959 replaced when Pirna 014 engines became available RD 9AK Non afterburning versions for the Yak 25 and Yak 26 RD 9AF 300 Afterburning version for the Yak 27 and Yak 28 RD 9AF2 300 Afterburning version for the Yak 27 and Yak 28 RD 9B Afterburning version for the early variants of MiG 19 RD 9BK Version for Lavochkin La 17M RD 9BF 811 Afterburning version for the later variants of MiG 19 RD 9V Afterburning version used in the Ilyushin Il 40P WP 6 Chinese built version for the Shenyang J 6 WP 6A a Chinese upgraded version for the Nanchang Q 5 and J 6C WP 6Z further developed for the cancelled Nanchang J 12 NK TJ i North Korean version built for MiG 19 and Shenyang J 6 3 Specifications RD 9BF 811 editData from 4 5 General characteristics Type Afterburning turbojet Length 5 560 mm 219 in Diameter 668 mm 26 in Dry weight 725 kg 1 600 lb Components Compressor Single spool 9 stage Axial compressor Turbine axial flowPerformance Maximum thrust 3 000 kgf 6 600 lbf 29 kN military power 3 750 kgf 8 300 lbf 37 kN with afterburner Turbine inlet temperature 860 C Specific fuel consumption 0 96 lb lbf h or 27 g kN s military power 1 6 lb lbf h or 45 g kN s afterburnerrner Thrust to weight ratio 5 2See also editComparable engines Allison J35 General Electric J47Related lists List of aircraft enginesNotes edit designation is just a placeholderReferences edit Belyakov R A Marmain J 1991 MiG 1939 1989 Paris Editions Lariviere p 137 ISBN 2 907051 00 8 Leonard Barry January 2011 History of Strategic and Ballistic Missile Defense Volume II DIANE Publishing p 245 ISBN 9781437921311 북한의 무인기 Mm 1 Mikulin AM 5 Tumansky RD 9 Wopen WP 6 Turboreaktivnyj dvigatel RD 9 The Osprey Encyclopedia of Russian Aircraft 1875 1995 Bill Gunston ISBN 1 85532 405 9 External links edit nbsp Wikimedia Commons has media related to Tumansky RD 9 RD 9B page on LeteckeMotory cz cs Retrieved from https en wikipedia org w index php title Tumansky RD 9 amp oldid 1178783598, wikipedia, wiki, book, books, library,

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