Dushkin S-155
Rocket motor
Country of origin | Soviet Union |
---|---|
Manufacturer | Dushkin OKB |
Application | Booster rocket for aircraft |
Liquid-fuel engine | |
Propellant | AK-20 (nitric acid) / TG-02 hypergolic kerosene |
Performance | |
Thrust, sea-level | 37.3 kN (8380 lbf) |
Dimensions | |
Dry mass | 1,100 lb |
The Dushkin S-155 was a liquid-fueled rocket motor designed by Leonid Dushkin specifically for use in the Mikoyan-Gurevich Ye-50 and Ye-50A (aka MiG-23U) experimental-developmental aircraft in the 1950s. It delivered 37.3 kN (8380 lbf) and ran on a mix of TG-02 hypergolic kerosene and AK-20 oxidizer (nitric acid). The fuel pumps were powered with grade T hydrogen peroxide.[1]
References
- ^ Gordon, Yefim "MiG-21" ISBN 978-1-85780-257-3
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Aviation rocket engines and rocket motors
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