| http://dbpedia.org/ontology/abstract
|
YF-40はN2O4とUDMHをガス発生器サイクルで燃焼する中国の液体燃料 ロケットエンジンである。2個のジンバル装架式燃焼室を備える。 原型機は長征1号Dの2段目のために開発された。 長征4号シリーズの3段目で使用される。
, The YF-40 is a Chinese liquid rocket engin … The YF-40 is a Chinese liquid rocket engine burning N2O4 and UDMH in a gas generator cycle. It has dual gimbaling combustion chambers. Originally it was developed for the Long March 1D second stage. It is used on the third stage of the Long March 4 family of launch vehicles.he Long March 4 family of launch vehicles.
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47248502
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4591
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1061626332
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http://dbpedia.org/resource/Gimbaled_thrust +
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--03-01
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|
412.0
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| http://dbpedia.org/property/combustionChamber
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2
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http://dbpedia.org/resource/China +
|
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|
http://dbpedia.org/resource/Gas-generator_cycle_%28rocket%29 +
|
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http://dbpedia.org/resource/Academy_of_Aerospace_Liquid_Propulsion_Technology +
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"1995-06-01"^^xsd:date
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| http://dbpedia.org/property/fuel
|
http://dbpedia.org/resource/Unsymmetrical_dimethylhydrazine +
|
| http://dbpedia.org/property/gimbal
|
±4.5°
|
| http://dbpedia.org/property/mixtureRatio
|
2.14
|
| http://dbpedia.org/property/name
|
YF-40B
|
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|
55
|
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|
http://dbpedia.org/resource/Dinitrogen_tetroxide +
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|
In Production
|
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|
liquid
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--03-01
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http://dbpedia.org/resource/Category:Rocket_engines_using_hypergolic_propellant +
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http://dbpedia.org/resource/O +
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http://en.wikipedia.org/wiki/YF-40 +
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http://www.wikidata.org/entity/Q20942882 +
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http://dbpedia.org/ontology/Person +
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| rdfs:comment |
YF-40はN2O4とUDMHをガス発生器サイクルで燃焼する中国の液体燃料 ロケットエンジンである。2個のジンバル装架式燃焼室を備える。 原型機は長征1号Dの2段目のために開発された。 長征4号シリーズの3段目で使用される。
, The YF-40 is a Chinese liquid rocket engin … The YF-40 is a Chinese liquid rocket engine burning N2O4 and UDMH in a gas generator cycle. It has dual gimbaling combustion chambers. Originally it was developed for the Long March 1D second stage. It is used on the third stage of the Long March 4 family of launch vehicles.he Long March 4 family of launch vehicles.
|
| rdfs:label |
YF-40
|
