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http://dbpedia.org/ontology/abstract The Dushkin S-155 was a liquid-fueled rockThe 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.re powered with grade T hydrogen peroxide. , Dushkin S-155 adalah sebuah motor mesin roDushkin S-155 adalah sebuah motor mesin roket berbahan bakar cair yang dirancang oleh Leonid Dushkin khusus untuk digunakan dalam pesawat eksperimental Mikoyan-Gurevich Ye-50 dan Ye-50A (alias MiG-23U) pada tahun 1950. Mesin ini menghasilkan daya dorong 37,3 kN (8380 lbf) dan berlari pada campuran minyak tanah hypergolic TG-02 dan oxidizer AK-20 (asam nitrat). Pompa bahan bakar didukung dengan hidrogen peroksida kelas T.idukung dengan hidrogen peroksida kelas T. , Le Douchkine S-155 était un moteur-fusée àLe Douchkine S-155 était un moteur-fusée à ergols liquides soviétique, conçu par (en) spécifiquement pour les avions de développement expérimentaux MiG E-50 et Yak-27V dans les années 1950. Il produisait une poussée de 37,3 kN et fonctionnait grâce à un mélange hypergolique de kérosène TG-02 et d'oxydant AK-20 (Acide nitrique). Les pompes à ergols étaient mises en fonction avec du peroxyde d'hydrogène de type « T ».vec du peroxyde d'hydrogène de type « T ».
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http://dbpedia.org/property/countryOfOrigin http://dbpedia.org/resource/Soviet_Union +
http://dbpedia.org/property/fuel TG-02 hypergolic kerosene
http://dbpedia.org/property/manufacturer http://dbpedia.org/resource/Dushkin_OKB +
http://dbpedia.org/property/name S-155
http://dbpedia.org/property/oxidiser AK-20
http://dbpedia.org/property/purpose Booster rocket for aircraft
http://dbpedia.org/property/thrust(sl)  37.3 kN
http://dbpedia.org/property/type liquid
http://dbpedia.org/property/weight 1100.0
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rdfs:comment Dushkin S-155 adalah sebuah motor mesin roDushkin S-155 adalah sebuah motor mesin roket berbahan bakar cair yang dirancang oleh Leonid Dushkin khusus untuk digunakan dalam pesawat eksperimental Mikoyan-Gurevich Ye-50 dan Ye-50A (alias MiG-23U) pada tahun 1950. Mesin ini menghasilkan daya dorong 37,3 kN (8380 lbf) dan berlari pada campuran minyak tanah hypergolic TG-02 dan oxidizer AK-20 (asam nitrat). Pompa bahan bakar didukung dengan hidrogen peroksida kelas T.idukung dengan hidrogen peroksida kelas T. , Le Douchkine S-155 était un moteur-fusée àLe Douchkine S-155 était un moteur-fusée à ergols liquides soviétique, conçu par (en) spécifiquement pour les avions de développement expérimentaux MiG E-50 et Yak-27V dans les années 1950. Il produisait une poussée de 37,3 kN et fonctionnait grâce à un mélange hypergolique de kérosène TG-02 et d'oxydant AK-20 (Acide nitrique). Les pompes à ergols étaient mises en fonction avec du peroxyde d'hydrogène de type « T ».vec du peroxyde d'hydrogène de type « T ». , The Dushkin S-155 was a liquid-fueled rockThe 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.re powered with grade T hydrogen peroxide.
rdfs:label Douchkine S-155 , Dushkin S-155
hide properties that link here 
http://dbpedia.org/resource/List_of_aircraft_engines + , http://dbpedia.org/resource/List_of_Mikoyan-Gurevich_MiG-21_variants + , http://dbpedia.org/resource/Yakovlev_Yak-27 + , http://dbpedia.org/resource/Dushkin + http://dbpedia.org/ontology/wikiPageWikiLink
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