avia.wikisort.org - Engine

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)
Designed by	Pyotr A. Kolesov

Variants and Applications

RD-36-35

• MiG-21PD[2]
• Mikoyan-Gurevich 23-01 (Mikoyan Guryevich E-7PD)[2]
• Sukhoi T-58VD[2]

RD-36-35PR

• Bartini Beriev VVA-14

RD-36-35F

• Bartini KOR-70 (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]

• Yakovlev Yak-38
• Yakovlev Yak-38U

RD-36-35K

• Mikoyan-Gurevich MiG-105

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

• Maximum thrust: 28.45 kN (6,396 lbf)
• Power-to-weight ratio:

References

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