Rybinsk RD-36-35

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Rybinsk RD-36-35
Type turbojet lift engine
National origin USSR
Manufacturer (RKBM)
Designed by

The Rybinsk RD-36-35 was a small lift turbojet engine, designed for use on V/STOL aircraft at the Rybinsk Engine Design Bureau (RKBM), designed by . Very little is known of this engine, probably due to confusion with the similarly designated Kolesov RD-36 and Lotarev D-36, which have little or no relation to the lift-jet.[1]

Variants and Applications[]

RD-36-35
RD-36-35PR
RD-36-35F
  • (Project for high speed VTOL ship-borne floatplane Kor.S)[3]
  • Yakovlev Yak-36M
  • Yakovlev Yak-38U
RD-36-35FV
(izdeliye 24) 28.45 kN (6,396 lbf)[1]
  • Yakovlev Yak-36M
RD-36-35FVR
(izdeliye 28) 29.9 kN (6,722 lbf)[1]
RD-36-35K

Specifications (RD-36-35FV)[]

Data from OKB Yakovlev[1]

General characteristics

  • Type: Lift turbojet/turbofan
  • Length:
  • Diameter:
  • Dry weight: 176 kg (388 lb) (RD-36-35F)

Components

  • Compressor: 6-stage axial
  • Turbine: 1-stage axial

Performance

References[]

  1. ^ a b c d Gordon, Yefim; Dmitry; Sergey Komissarov (2005). OKB Yakovlev. Hinkley: Midland Publishing. pp. 334-342. ISBN 1-85780-203-9.
  2. ^ a b c “Engine” No. 4/2007 // Alexander Nikolaev “We take off vertically!”
  3. ^ “” No. 9/2001 // Vyacheslav Zayarin, Konstantin Udalov “The Concept of the Universal Vertical
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