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- Dushkin_S-155 abstract "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.".
- Dushkin_S-155 wikiPageID "21850291".
- Dushkin_S-155 wikiPageRevisionID "602051774".
- Dushkin_S-155 countryOfOrigin Soviet_Union.
- Dushkin_S-155 fuel "TG-02 hypergolic kerosene".
- Dushkin_S-155 hasPhotoCollection Dushkin_S-155.
- Dushkin_S-155 manufacturer Dushkin_OKB.
- Dushkin_S-155 name "S-155".
- Dushkin_S-155 oxidiser "AK-20".
- Dushkin_S-155 purpose "Booster rocket for aircraft".
- Dushkin_S-155 thrust(sl)_ "37.3 kN".
- Dushkin_S-155 type "liquid".
- Dushkin_S-155 weight "1100.0".
- Dushkin_S-155 subject Category:Kerosene_rocket_engines.
- Dushkin_S-155 subject Category:Rocket_engines.
- Dushkin_S-155 comment "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.".
- Dushkin_S-155 label "Dushkin S-155".
- Dushkin_S-155 sameAs Dushkin_S-155.
- Dushkin_S-155 sameAs m.05p31bz.
- Dushkin_S-155 sameAs Q5316884.
- Dushkin_S-155 sameAs Q5316884.
- Dushkin_S-155 wasDerivedFrom Dushkin_S-155?oldid=602051774.
- Dushkin_S-155 isPrimaryTopicOf Dushkin_S-155.