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Engine RD-9B |
Soviet turbojet with axial compressor and afterburner.
Engine RD-9 was firs turbojet completely developed in Soviet Union in OKB Mikulin. First version was designated AM-5. Later with modified compressor named AM-9. When chief designer was replaced in 1956 from Tumansky to Mikulin engine was renamed to RD-9.
RD-9A, RD-9AK - engine without afterburner chamber used in Yak-25M and Yak-26 (engine thrust 27,46 kN)
RD-9АF-300, RD-9-АF2-300 - engine with afterburner used in Yak-27 a Yak-28.
RD-9B - engine with afterburner used in earlier versions of MiG-19.
RD-9BF-811 - basic afterburner version used in MiG-19.
Basic technical specifications of the RD-9B: |
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| dry mass: | 659 kg |
| diameter: | 0,665 m |
| length: | 5,555 m |
| total pressure ratio: | 7,14 |
| air mass flow: | 45,3 kg/s |
| specific fuel consumption: | 0,09 kg/N/h |
| specific fuel consumption with afterburner: | 0,169 kg/N/h |
| turbine entry temperature: | 860 °C |
| rpm: | 11150/min |
| engine thrust: | 25,51 kN |
| engine thrust: with afterburner: | 31,90 kN |
© Kamil Pankuch 2004-2007
airmuseum.kosice at gmail.com
