Rybinsk RD-36-35

(Redirected from Rybinsk RD-38)

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 Pyotr A. Kolesov. 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]

Rybinsk RD-36-35
Type turbojet lift engine
National origin USSR
Manufacturer Rybinsk Engine Design Bureau (RKBM)
Designer Pyotr A. Kolesov

Variants and Applications

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RD-36-35
RD-36-35PR
RD-36-35F
RD-36-35FV
(izdeliye 24) 28.45 kN (6,396 lbf)[1]
RD-36-35FVR
(izdeliye 28) 29.9 kN (6,722 lbf)[1]
RD-36-35K

Specifications (RD-36-35FV)

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Data from OKB Yakovlev[1]

General characteristics

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

Components

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

Performance

  • Maximum thrust: 28.45 kN (6,396 lbf)

References

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  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. ^ Wings of the Motherland” No. 9/2001 // Vyacheslav Zayarin, Konstantin Udalov “The Concept of the Universal Vertical