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]
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
- 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]
- 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
- 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
- ^ a b c d Gordon, Yefim; Dmitry; Sergey Komissarov (2005). OKB Yakovlev. Hinkley: Midland Publishing. pp. 334-342. ISBN 1-85780-203-9.
- ^ a b c “Engine” No. 4/2007 // Alexander Nikolaev “We take off vertically!”
- ^ “Wings of the Motherland” No. 9/2001 // Vyacheslav Zayarin, Konstantin Udalov “The Concept of the Universal Vertical
This page was last edited on 8 January 2024, at 14:51