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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 wikiPageLength "1201".
- Dushkin_S-155 wikiPageOutDegree "11".
- Dushkin_S-155 wikiPageRevisionID "671915374".
- Dushkin_S-155 wikiPageWikiLink Category:Aircraft_rocket_engines.
- Dushkin_S-155 wikiPageWikiLink Category:Rocket_engines_using_hypergolic_propellant.
- Dushkin_S-155 wikiPageWikiLink Category:Rocket_engines_using_kerosene_propellant.
- Dushkin_S-155 wikiPageWikiLink Dushkin_OKB.
- Dushkin_S-155 wikiPageWikiLink Hypergolic.
- Dushkin_S-155 wikiPageWikiLink Hypergolic_propellant.
- Dushkin_S-155 wikiPageWikiLink Kerosene.
- Dushkin_S-155 wikiPageWikiLink Leonid_Dushkin.
- Dushkin_S-155 wikiPageWikiLink List_of_Mikoyan-Gurevich_MiG-21_variants.
- Dushkin_S-155 wikiPageWikiLink Mikoyan.
- Dushkin_S-155 wikiPageWikiLink Mikoyan-Gurevich.
- Dushkin_S-155 wikiPageWikiLink Mikoyan-Gurevich_MiG-21_Variants_-_Development_and_Preproduction.
- Dushkin_S-155 wikiPageWikiLink Nitric_acid.
- Dushkin_S-155 wikiPageWikiLink Soviet_Union.
- Dushkin_S-155 wikiPageWikiLinkText "Dushkin S-155".
- 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 wikiPageUsesTemplate Template:Aviation_rocket_engines.
- Dushkin_S-155 wikiPageUsesTemplate Template:Engine-aircraft-stub.
- Dushkin_S-155 wikiPageUsesTemplate Template:Infobox_rocket_engine.
- Dushkin_S-155 wikiPageUsesTemplate Template:Reflist.
- Dushkin_S-155 subject Category:Aircraft_rocket_engines.
- Dushkin_S-155 subject Category:Rocket_engines_using_hypergolic_propellant.
- Dushkin_S-155 subject Category:Rocket_engines_using_kerosene_propellant.
- Dushkin_S-155 hypernym Motor.
- Dushkin_S-155 type Person.
- 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=671915374.
- Dushkin_S-155 isPrimaryTopicOf Dushkin_S-155.